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You searched for +publisher:"Indian Institute of Science" +contributor:("Raghunandan, B N"). Showing records 1 – 16 of 16 total matches.

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Indian Institute of Science

1. Lal, Amit. Onboard Propellant Gauging For Spacecraft.

Degree: 2007, Indian Institute of Science

 Estimation of the total mission life of a spacecraft is an important issue for the communication satellite industries. For accurate determination of the remaining mission… (more)

Subjects/Keywords: Spacecraft - Propellants; Propellant Gauging; Gas Injection Method; Book-Keeping Method; Propellant Tank Heating Method; Uncertainty Analysis; Onboard Propellant; Astronautics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Lal, A. (2007). Onboard Propellant Gauging For Spacecraft. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/355

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Lal, Amit. “Onboard Propellant Gauging For Spacecraft.” 2007. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/355.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Lal, Amit. “Onboard Propellant Gauging For Spacecraft.” 2007. Web. 15 Feb 2019.

Vancouver:

Lal A. Onboard Propellant Gauging For Spacecraft. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/355.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Lal A. Onboard Propellant Gauging For Spacecraft. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/355

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

2. Gadgil, Hrishikesh Prabhakar. Studies On Impinging-Jet Atomizers.

Degree: 2007, Indian Institute of Science

 Characteristics of impinging-jet atomizers in the context of application in liquid propulsion systems are studied in this thesis. A review of past studies on impinging… (more)

Subjects/Keywords: Jet Engines; Liquid Propulsion; Combustion; Liquid Propellant Rockets - Atomization; Skewed Jets; Impinging Jets; Jet Atomizers; Sauter Mean Diameter (SMD); Heat Engineering

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Gadgil, H. P. (2007). Studies On Impinging-Jet Atomizers. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/485

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Gadgil, Hrishikesh Prabhakar. “Studies On Impinging-Jet Atomizers.” 2007. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/485.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Gadgil, Hrishikesh Prabhakar. “Studies On Impinging-Jet Atomizers.” 2007. Web. 15 Feb 2019.

Vancouver:

Gadgil HP. Studies On Impinging-Jet Atomizers. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/485.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Gadgil HP. Studies On Impinging-Jet Atomizers. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/485

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

3. Lal, Amit. Onboard Propellant Gauging For Spacecraft.

Degree: 2007, Indian Institute of Science

 Estimation of the total mission life of a spacecraft is an important issue for the communication satellite industries. For accurate determination of the remaining mission… (more)

Subjects/Keywords: Spacecraft - Propellants; Propellant Gauging; Gas Injection Method; Book-Keeping Method; Propellant Tank Heating Method; Aerospace Propulsion; Uncertainty Analysis; Astronautics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Lal, A. (2007). Onboard Propellant Gauging For Spacecraft. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/579

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Lal, Amit. “Onboard Propellant Gauging For Spacecraft.” 2007. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/579.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Lal, Amit. “Onboard Propellant Gauging For Spacecraft.” 2007. Web. 15 Feb 2019.

Vancouver:

Lal A. Onboard Propellant Gauging For Spacecraft. [Internet] [Thesis]. Indian Institute of Science; 2007. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/579.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Lal A. Onboard Propellant Gauging For Spacecraft. [Thesis]. Indian Institute of Science; 2007. Available from: http://hdl.handle.net/2005/579

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

4. Srinivasan, R. Momentum And Enthalpy Transfer In Packed Beds - Experimental Evaluation For Unsteady Inlet Temperature At High Reynolds Numbers.

Degree: 2010, Indian Institute of Science

 Solid propellant gas generators that have high gas capacity are used for fast pressurization of inflatable devices or elastic shells. However, many applications such as… (more)

Subjects/Keywords: Applied Thermodynamics; Enthalpy; Reynolds Number; Heat Transfer; Packed Beds; Nusselt Number; High Reynolds Numbers; Momentum; Heat Engineering

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APA (6th Edition):

Srinivasan, R. (2010). Momentum And Enthalpy Transfer In Packed Beds - Experimental Evaluation For Unsteady Inlet Temperature At High Reynolds Numbers. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2034

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Srinivasan, R. “Momentum And Enthalpy Transfer In Packed Beds - Experimental Evaluation For Unsteady Inlet Temperature At High Reynolds Numbers.” 2010. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/2034.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Srinivasan, R. “Momentum And Enthalpy Transfer In Packed Beds - Experimental Evaluation For Unsteady Inlet Temperature At High Reynolds Numbers.” 2010. Web. 15 Feb 2019.

Vancouver:

Srinivasan R. Momentum And Enthalpy Transfer In Packed Beds - Experimental Evaluation For Unsteady Inlet Temperature At High Reynolds Numbers. [Internet] [Thesis]. Indian Institute of Science; 2010. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/2034.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Srinivasan R. Momentum And Enthalpy Transfer In Packed Beds - Experimental Evaluation For Unsteady Inlet Temperature At High Reynolds Numbers. [Thesis]. Indian Institute of Science; 2010. Available from: http://hdl.handle.net/2005/2034

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

5. Bhaskaran, Ramprasad. Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source.

Degree: 2012, Indian Institute of Science

 Stirling engines are promising candidates for applications where air breathing engines cannot be used. Self contained engines capable of operating independently of the environment are… (more)

Subjects/Keywords: Free-Piston Sterling Engine; Sterling Engine; Spacecraft - Sterling Engine; Space Power Generation; Free-Piston Sterling Engine - Parametric Analysis; Spacecraft - Radioisotope Heat Source; Free Piston Stirling Engine; Heat Engineering

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Bhaskaran, R. (2012). Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/2339

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Bhaskaran, Ramprasad. “Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source.” 2012. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/2339.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Bhaskaran, Ramprasad. “Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source.” 2012. Web. 15 Feb 2019.

Vancouver:

Bhaskaran R. Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/2339.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bhaskaran R. Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source. [Thesis]. Indian Institute of Science; 2012. Available from: http://hdl.handle.net/2005/2339

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

6. Bhaskaran, Ramprasad. Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source.

Degree: 2012, Indian Institute of Science

 Stirling engines are promising candidates for applications where air breathing engines cannot be used. Self contained engines capable of operating independently of the environment are… (more)

Subjects/Keywords: Free-Piston Sterling Engine; Sterling Engine; Spacecraft - Sterling Engine; Space Power Generation; Free-Piston Sterling Engine - Parametric Analysis; Spacecraft - Radioisotope Heat Source; Free Piston Stirling Engine; Heat Engineering

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Bhaskaran, R. (2012). Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/2339 ; http://etd.ncsi.iisc.ernet.in/abstracts/3009/G25328-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Bhaskaran, Ramprasad. “Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source.” 2012. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://etd.iisc.ernet.in/handle/2005/2339 ; http://etd.ncsi.iisc.ernet.in/abstracts/3009/G25328-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Bhaskaran, Ramprasad. “Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source.” 2012. Web. 15 Feb 2019.

Vancouver:

Bhaskaran R. Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source. [Internet] [Thesis]. Indian Institute of Science; 2012. [cited 2019 Feb 15]. Available from: http://etd.iisc.ernet.in/handle/2005/2339 ; http://etd.ncsi.iisc.ernet.in/abstracts/3009/G25328-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bhaskaran R. Parametric Analysis Of A Free Piston Stirling Engine For Spacecraft Power Applications With A Radioisotope Heat Source. [Thesis]. Indian Institute of Science; 2012. Available from: http://etd.iisc.ernet.in/handle/2005/2339 ; http://etd.ncsi.iisc.ernet.in/abstracts/3009/G25328-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

7. Aatresh, K. Microgravity Flow Transients in the Context of On-Board Propellant Gauging.

Degree: 2014, Indian Institute of Science

 It is well known that surface tension of a liquid has a decisive role in flow dynamics and the eventual equilibrium state, especially in confined… (more)

Subjects/Keywords: Spacecraft Propellant; Microgravity Flow Transients; Propellant Gauging; Volume Fraction Equation; Surface Tension Model; ANSYS FLUENT; Surface Tension; Volume of Fluid (VOF); Aerospace Engineering

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Aatresh, K. (2014). Microgravity Flow Transients in the Context of On-Board Propellant Gauging. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/3105

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Aatresh, K. “Microgravity Flow Transients in the Context of On-Board Propellant Gauging.” 2014. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/3105.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Aatresh, K. “Microgravity Flow Transients in the Context of On-Board Propellant Gauging.” 2014. Web. 15 Feb 2019.

Vancouver:

Aatresh K. Microgravity Flow Transients in the Context of On-Board Propellant Gauging. [Internet] [Thesis]. Indian Institute of Science; 2014. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/3105.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Aatresh K. Microgravity Flow Transients in the Context of On-Board Propellant Gauging. [Thesis]. Indian Institute of Science; 2014. Available from: http://hdl.handle.net/2005/3105

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

8. Rakesh, P. A Study of the Characteristics of Gas-On-Liquid Impinging Injectors.

Degree: 2014, Indian Institute of Science

 The work presented here pertains to investigations on gas-on-liquid type of impinging injectors with a generic approach with prospective applications in several areas, and at… (more)

Subjects/Keywords: Impinging Injectors; Impinging Atomizers; Gas-On-Liquid Impinging Injectors; Liquid Propellant Rockets; Impinging Jet Injectors; Atomizers; Cryogenic Rocket Injectors; Impinging Fuel Injector Atomization; Impinging Injectors Spraying; Image Processing - Spraying; Gas-On-Liquid Impinging Sprays; Liquid-on Liquid Impingement; Aerospace Engineering

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APA (6th Edition):

Rakesh, P. (2014). A Study of the Characteristics of Gas-On-Liquid Impinging Injectors. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/3126

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Rakesh, P. “A Study of the Characteristics of Gas-On-Liquid Impinging Injectors.” 2014. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/3126.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Rakesh, P. “A Study of the Characteristics of Gas-On-Liquid Impinging Injectors.” 2014. Web. 15 Feb 2019.

Vancouver:

Rakesh P. A Study of the Characteristics of Gas-On-Liquid Impinging Injectors. [Internet] [Thesis]. Indian Institute of Science; 2014. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/3126.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Rakesh P. A Study of the Characteristics of Gas-On-Liquid Impinging Injectors. [Thesis]. Indian Institute of Science; 2014. Available from: http://hdl.handle.net/2005/3126

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

9. Hiremath, Rahul B. Decentralized Sustainable Energy Planning For Tumkur District, India.

Degree: 2009, Indian Institute of Science

 The energy-planning involves finding a set of sources and conversion devices so as to meet the energy requirements/demands of all the activities in an optimal… (more)

Subjects/Keywords: Energy Resources - Planning - India; Energy Resources - Planning - Karnataka; Energy Resources - Planning - Tumkur; Decentralized Energy Planning (DEP); Energy And Environmental Planning - Models; Sustainable Development; Biomass Energy; Energy Economics

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APA (6th Edition):

Hiremath, R. B. (2009). Decentralized Sustainable Energy Planning For Tumkur District, India. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/641

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Hiremath, Rahul B. “Decentralized Sustainable Energy Planning For Tumkur District, India.” 2009. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/641.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Hiremath, Rahul B. “Decentralized Sustainable Energy Planning For Tumkur District, India.” 2009. Web. 15 Feb 2019.

Vancouver:

Hiremath RB. Decentralized Sustainable Energy Planning For Tumkur District, India. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/641.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Hiremath RB. Decentralized Sustainable Energy Planning For Tumkur District, India. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/641

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

10. Allamaprabhu, Yaravintelimath. Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles.

Degree: 2014, Indian Institute of Science

 Convergent-Divergent (C-D) nozzles are used in rocket engines to produce thrust as a reaction to the acceleration of hot combustion chamber gases in the opposite… (more)

Subjects/Keywords: Rocket Nozzles; Nozzle Flow Seperation; Turbulence Modeling; Contoured Rocket Nozzles; Rocket Nozzle Flow Seperation - Numerical Simulation; Reynolds Averaged Navier-stokes (RANS) Simulations; Spalart-Allmaras (SA) Turbulence Model; Shear Stress Transport (SST) Turbulence Model; Rocket Nozzle Contours; Shear Stress Transport; SST Model; Aerospace Engineering

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APA (6th Edition):

Allamaprabhu, Y. (2014). Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/3046

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Allamaprabhu, Yaravintelimath. “Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles.” 2014. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/3046.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Allamaprabhu, Yaravintelimath. “Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles.” 2014. Web. 15 Feb 2019.

Vancouver:

Allamaprabhu Y. Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles. [Internet] [Thesis]. Indian Institute of Science; 2014. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/3046.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Allamaprabhu Y. Turbulence Modeling for Predicting Flow Separation in Rocket Nozzles. [Thesis]. Indian Institute of Science; 2014. Available from: http://hdl.handle.net/2005/3046

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

11. Ganu, Hrishikesh Vidyadhar. A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays.

Degree: 2005, Indian Institute of Science

Subjects/Keywords: Cryogenic Sprays; Atomization; Cryogenic Sprays - Drop Sizing; Cryogenic Sprays - Quantifying; Cryogenic Spray Breakup; Liquid Propellant Rocket Engines; Spray Characterization; Cryogenics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Ganu, H. V. (2005). A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1481

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Ganu, Hrishikesh Vidyadhar. “A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays.” 2005. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/1481.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Ganu, Hrishikesh Vidyadhar. “A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays.” 2005. Web. 15 Feb 2019.

Vancouver:

Ganu HV. A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays. [Internet] [Thesis]. Indian Institute of Science; 2005. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/1481.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ganu HV. A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays. [Thesis]. Indian Institute of Science; 2005. Available from: http://hdl.handle.net/2005/1481

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

12. Parthiban, S. Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion.

Degree: 1996, Indian Institute of Science

Subjects/Keywords: Ozone Depletion; Chlorine Compounds; Nitric Oxide; N2O5; Stratospheric Ozone; Dichlorine Hexoxide; Dichlorine Heptoxide; Dinitrogen Pentoxide; Ozone Layer; Meteorology

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APA (6th Edition):

Parthiban, S. (1996). Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1574

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Parthiban, S. “Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion.” 1996. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/1574.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Parthiban, S. “Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion.” 1996. Web. 15 Feb 2019.

Vancouver:

Parthiban S. Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion. [Internet] [Thesis]. Indian Institute of Science; 1996. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/1574.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Parthiban S. Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion. [Thesis]. Indian Institute of Science; 1996. Available from: http://hdl.handle.net/2005/1574

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

13. Amirthaganesh, S. Heat Transfer And Combustion In Baffle Separated Flows.

Degree: 1996, Indian Institute of Science

Subjects/Keywords: Combustion; Airflow; Heat Transmission; Baffle Separated Flow; Natural Convection; Baffle Mounted Surface; Aerodynamics

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APA (6th Edition):

Amirthaganesh, S. (1996). Heat Transfer And Combustion In Baffle Separated Flows. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1577

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Amirthaganesh, S. “Heat Transfer And Combustion In Baffle Separated Flows.” 1996. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://hdl.handle.net/2005/1577.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Amirthaganesh, S. “Heat Transfer And Combustion In Baffle Separated Flows.” 1996. Web. 15 Feb 2019.

Vancouver:

Amirthaganesh S. Heat Transfer And Combustion In Baffle Separated Flows. [Internet] [Thesis]. Indian Institute of Science; 1996. [cited 2019 Feb 15]. Available from: http://hdl.handle.net/2005/1577.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Amirthaganesh S. Heat Transfer And Combustion In Baffle Separated Flows. [Thesis]. Indian Institute of Science; 1996. Available from: http://hdl.handle.net/2005/1577

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

14. Ganu, Hrishikesh Vidyadhar. A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays.

Degree: 2005, Indian Institute of Science

Subjects/Keywords: Cryogenic Sprays; Atomization; Cryogenic Sprays - Drop Sizing; Cryogenic Sprays - Quantifying; Cryogenic Spray Breakup; Liquid Propellant Rocket Engines; Spray Characterization; Cryogenics

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Ganu, H. V. (2005). A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/1481 ; http://etd.ncsi.iisc.ernet.in/abstracts/1901/G19602-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Ganu, Hrishikesh Vidyadhar. “A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays.” 2005. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://etd.iisc.ernet.in/handle/2005/1481 ; http://etd.ncsi.iisc.ernet.in/abstracts/1901/G19602-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Ganu, Hrishikesh Vidyadhar. “A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays.” 2005. Web. 15 Feb 2019.

Vancouver:

Ganu HV. A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays. [Internet] [Thesis]. Indian Institute of Science; 2005. [cited 2019 Feb 15]. Available from: http://etd.iisc.ernet.in/handle/2005/1481 ; http://etd.ncsi.iisc.ernet.in/abstracts/1901/G19602-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ganu HV. A Morphological Technique For Direct Drop Size Measurement Of Cryogenic Sprays. [Thesis]. Indian Institute of Science; 2005. Available from: http://etd.iisc.ernet.in/handle/2005/1481 ; http://etd.ncsi.iisc.ernet.in/abstracts/1901/G19602-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

15. Parthiban, S. Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion.

Degree: 1996, Indian Institute of Science

Subjects/Keywords: Ozone Depletion; Chlorine Compounds; Nitric Oxide; N2O5; Stratospheric Ozone; Dichlorine Hexoxide; Dichlorine Heptoxide; Dinitrogen Pentoxide; Ozone Layer; Meteorology

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Parthiban, S. (1996). Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/1574 ; http://etd.ncsi.iisc.ernet.in/abstracts/2011/G14532-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Parthiban, S. “Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion.” 1996. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://etd.iisc.ernet.in/handle/2005/1574 ; http://etd.ncsi.iisc.ernet.in/abstracts/2011/G14532-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Parthiban, S. “Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion.” 1996. Web. 15 Feb 2019.

Vancouver:

Parthiban S. Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion. [Internet] [Thesis]. Indian Institute of Science; 1996. [cited 2019 Feb 15]. Available from: http://etd.iisc.ernet.in/handle/2005/1574 ; http://etd.ncsi.iisc.ernet.in/abstracts/2011/G14532-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Parthiban S. Theoretical Studies Of XOClO3 (X-ClO2, ClO3, Cl, F And H) And N2O5 : Implications For Stratospheric Ozone Depletion. [Thesis]. Indian Institute of Science; 1996. Available from: http://etd.iisc.ernet.in/handle/2005/1574 ; http://etd.ncsi.iisc.ernet.in/abstracts/2011/G14532-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


Indian Institute of Science

16. Amirthaganesh, S. Heat Transfer And Combustion In Baffle Separated Flows.

Degree: 1996, Indian Institute of Science

Subjects/Keywords: Combustion; Airflow; Heat Transmission; Baffle Separated Flow; Natural Convection; Baffle Mounted Surface; Aerodynamics

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Amirthaganesh, S. (1996). Heat Transfer And Combustion In Baffle Separated Flows. (Thesis). Indian Institute of Science. Retrieved from http://etd.iisc.ernet.in/handle/2005/1577 ; http://etd.ncsi.iisc.ernet.in/abstracts/2014/G14500-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Amirthaganesh, S. “Heat Transfer And Combustion In Baffle Separated Flows.” 1996. Thesis, Indian Institute of Science. Accessed February 15, 2019. http://etd.iisc.ernet.in/handle/2005/1577 ; http://etd.ncsi.iisc.ernet.in/abstracts/2014/G14500-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Amirthaganesh, S. “Heat Transfer And Combustion In Baffle Separated Flows.” 1996. Web. 15 Feb 2019.

Vancouver:

Amirthaganesh S. Heat Transfer And Combustion In Baffle Separated Flows. [Internet] [Thesis]. Indian Institute of Science; 1996. [cited 2019 Feb 15]. Available from: http://etd.iisc.ernet.in/handle/2005/1577 ; http://etd.ncsi.iisc.ernet.in/abstracts/2014/G14500-Abs.pdf.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Amirthaganesh S. Heat Transfer And Combustion In Baffle Separated Flows. [Thesis]. Indian Institute of Science; 1996. Available from: http://etd.iisc.ernet.in/handle/2005/1577 ; http://etd.ncsi.iisc.ernet.in/abstracts/2014/G14500-Abs.pdf

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

.