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You searched for +publisher:"Embry-Riddle Aeronautical University" +contributor:("Dr. James Ladesic"). Showing records 1 – 8 of 8 total matches.

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Embry-Riddle Aeronautical University

1. Kazeneh, Ali. Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet.

Degree: Master of Aerospace Engineering, Aerospace Engineering, 2008, Embry-Riddle Aeronautical University

  The wing sweep schedule for the Gulfstream Quiet Supersonic Jet (wing and body) was investigated using CFD analysis methods. The use of automating the… (more)

Subjects/Keywords: Aerospace Engineering; Systems Engineering and Multidisciplinary Design Optimization

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APA (6th Edition):

Kazeneh, A. (2008). Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/95

Chicago Manual of Style (16th Edition):

Kazeneh, Ali. “Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet.” 2008. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/95.

MLA Handbook (7th Edition):

Kazeneh, Ali. “Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet.” 2008. Web. 23 Jan 2020.

Vancouver:

Kazeneh A. Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2008. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/95.

Council of Science Editors:

Kazeneh A. Development of Automatic CFD Grid Generation for the Design of the Preliminary Wing Sweep Schedule for the Gulfstream Quiet Supersonic Jet. [Masters Thesis]. Embry-Riddle Aeronautical University; 2008. Available from: https://commons.erau.edu/db-theses/95


Embry-Riddle Aeronautical University

2. Maerz, Stephen Jerry. Thermally Induced Vibration of a Cross-Ply Laminated Plate with Hygrothermal Effects (Exact Solution).

Degree: MSin Aerospace Engineering, Graduate Studies, 1992, Embry-Riddle Aeronautical University

  Of increasing importance in structural design is the use of fiber-reinforced polymeric composite material, notably in advanced aircraft and projectiles. These applications expose the… (more)

Subjects/Keywords: Aerospace Engineering

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APA (6th Edition):

Maerz, S. J. (1992). Thermally Induced Vibration of a Cross-Ply Laminated Plate with Hygrothermal Effects (Exact Solution). (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/262

Chicago Manual of Style (16th Edition):

Maerz, Stephen Jerry. “Thermally Induced Vibration of a Cross-Ply Laminated Plate with Hygrothermal Effects (Exact Solution).” 1992. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/262.

MLA Handbook (7th Edition):

Maerz, Stephen Jerry. “Thermally Induced Vibration of a Cross-Ply Laminated Plate with Hygrothermal Effects (Exact Solution).” 1992. Web. 23 Jan 2020.

Vancouver:

Maerz SJ. Thermally Induced Vibration of a Cross-Ply Laminated Plate with Hygrothermal Effects (Exact Solution). [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 1992. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/262.

Council of Science Editors:

Maerz SJ. Thermally Induced Vibration of a Cross-Ply Laminated Plate with Hygrothermal Effects (Exact Solution). [Masters Thesis]. Embry-Riddle Aeronautical University; 1992. Available from: https://commons.erau.edu/db-theses/262


Embry-Riddle Aeronautical University

3. Hinton, Michael J. Design and Construction of a 1/3-Scale, 1986 Cessna 172P Flight-Test Aircraft.

Degree: Master of Aerospace Engineering, Aerospace Engineering, 2001, Embry-Riddle Aeronautical University

  The incredible cost of prototype flight testing can be a very limiting factor in the optimization of new designs as they proceed from the… (more)

Subjects/Keywords: Aerospace Engineering

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APA (6th Edition):

Hinton, M. J. (2001). Design and Construction of a 1/3-Scale, 1986 Cessna 172P Flight-Test Aircraft. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/82

Chicago Manual of Style (16th Edition):

Hinton, Michael J. “Design and Construction of a 1/3-Scale, 1986 Cessna 172P Flight-Test Aircraft.” 2001. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/82.

MLA Handbook (7th Edition):

Hinton, Michael J. “Design and Construction of a 1/3-Scale, 1986 Cessna 172P Flight-Test Aircraft.” 2001. Web. 23 Jan 2020.

Vancouver:

Hinton MJ. Design and Construction of a 1/3-Scale, 1986 Cessna 172P Flight-Test Aircraft. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2001. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/82.

Council of Science Editors:

Hinton MJ. Design and Construction of a 1/3-Scale, 1986 Cessna 172P Flight-Test Aircraft. [Masters Thesis]. Embry-Riddle Aeronautical University; 2001. Available from: https://commons.erau.edu/db-theses/82


Embry-Riddle Aeronautical University

4. Njenga, Charles. Implementation of a Low Cost Micro Electro Mechanical Systems Inertial Navigation Solution.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2008, Embry-Riddle Aeronautical University

  The purpose of this study is to develop a low cost navigation solution for General Aviation (GA) aircraft and flight testing aircraft. This low… (more)

Subjects/Keywords: Aerospace Engineering

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APA (6th Edition):

Njenga, C. (2008). Implementation of a Low Cost Micro Electro Mechanical Systems Inertial Navigation Solution. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/158

Chicago Manual of Style (16th Edition):

Njenga, Charles. “Implementation of a Low Cost Micro Electro Mechanical Systems Inertial Navigation Solution.” 2008. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/158.

MLA Handbook (7th Edition):

Njenga, Charles. “Implementation of a Low Cost Micro Electro Mechanical Systems Inertial Navigation Solution.” 2008. Web. 23 Jan 2020.

Vancouver:

Njenga C. Implementation of a Low Cost Micro Electro Mechanical Systems Inertial Navigation Solution. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2008. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/158.

Council of Science Editors:

Njenga C. Implementation of a Low Cost Micro Electro Mechanical Systems Inertial Navigation Solution. [Masters Thesis]. Embry-Riddle Aeronautical University; 2008. Available from: https://commons.erau.edu/db-theses/158


Embry-Riddle Aeronautical University

5. Kriskovich, Horacio Esteban Sepic. The Effects of Elasticity in the Foundation on the Flutter of a Metallic High Aspect Ratio Wing.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 2009, Embry-Riddle Aeronautical University

  The goal of this thesis is to study the flutter characteristics of a metallic high-aspect ratio wing, with linearly varying chord across the semis-span,… (more)

Subjects/Keywords: Aerospace Engineering

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APA (6th Edition):

Kriskovich, H. E. S. (2009). The Effects of Elasticity in the Foundation on the Flutter of a Metallic High Aspect Ratio Wing. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/107

Chicago Manual of Style (16th Edition):

Kriskovich, Horacio Esteban Sepic. “The Effects of Elasticity in the Foundation on the Flutter of a Metallic High Aspect Ratio Wing.” 2009. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/107.

MLA Handbook (7th Edition):

Kriskovich, Horacio Esteban Sepic. “The Effects of Elasticity in the Foundation on the Flutter of a Metallic High Aspect Ratio Wing.” 2009. Web. 23 Jan 2020.

Vancouver:

Kriskovich HES. The Effects of Elasticity in the Foundation on the Flutter of a Metallic High Aspect Ratio Wing. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2009. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/107.

Council of Science Editors:

Kriskovich HES. The Effects of Elasticity in the Foundation on the Flutter of a Metallic High Aspect Ratio Wing. [Masters Thesis]. Embry-Riddle Aeronautical University; 2009. Available from: https://commons.erau.edu/db-theses/107


Embry-Riddle Aeronautical University

6. Peterson, Gary A. A Kinematical Investigation of Some External Wind Tunnel Force Measurement Systems.

Degree: MSin Aeronautical Engineering, Graduate Studies, 1988, Embry-Riddle Aeronautical University

  A discussion on the fundamental concepts associated with wind tunnel forces measurement systems (balances) is presented. Detailed static analyses are performed on the six… (more)

Subjects/Keywords: Aerospace Engineering

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APA (6th Edition):

Peterson, G. A. (1988). A Kinematical Investigation of Some External Wind Tunnel Force Measurement Systems. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/241

Chicago Manual of Style (16th Edition):

Peterson, Gary A. “A Kinematical Investigation of Some External Wind Tunnel Force Measurement Systems.” 1988. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/241.

MLA Handbook (7th Edition):

Peterson, Gary A. “A Kinematical Investigation of Some External Wind Tunnel Force Measurement Systems.” 1988. Web. 23 Jan 2020.

Vancouver:

Peterson GA. A Kinematical Investigation of Some External Wind Tunnel Force Measurement Systems. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 1988. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/241.

Council of Science Editors:

Peterson GA. A Kinematical Investigation of Some External Wind Tunnel Force Measurement Systems. [Masters Thesis]. Embry-Riddle Aeronautical University; 1988. Available from: https://commons.erau.edu/db-theses/241


Embry-Riddle Aeronautical University

7. Holt, Ryan Timothy. An Investigation of Classical Panel Stiffener Buckling Methods for Modern Airframe Applications.

Degree: Master of Aerospace Engineering, Aerospace Engineering, 2008, Embry-Riddle Aeronautical University

  Classical methods for buckling assessment of aircraft panels reinforced by bulb-stiffened flanges differ regarding symmetric versus asymmetric cross-sections. The present research addresses a number… (more)

Subjects/Keywords: Aerospace Engineering

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APA (6th Edition):

Holt, R. T. (2008). An Investigation of Classical Panel Stiffener Buckling Methods for Modern Airframe Applications. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/86

Chicago Manual of Style (16th Edition):

Holt, Ryan Timothy. “An Investigation of Classical Panel Stiffener Buckling Methods for Modern Airframe Applications.” 2008. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/86.

MLA Handbook (7th Edition):

Holt, Ryan Timothy. “An Investigation of Classical Panel Stiffener Buckling Methods for Modern Airframe Applications.” 2008. Web. 23 Jan 2020.

Vancouver:

Holt RT. An Investigation of Classical Panel Stiffener Buckling Methods for Modern Airframe Applications. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 2008. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/86.

Council of Science Editors:

Holt RT. An Investigation of Classical Panel Stiffener Buckling Methods for Modern Airframe Applications. [Masters Thesis]. Embry-Riddle Aeronautical University; 2008. Available from: https://commons.erau.edu/db-theses/86


Embry-Riddle Aeronautical University

8. Kaplan, Brian J. The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel.

Degree: MSin Aerospace Engineering, Aerospace Engineering, 1996, Embry-Riddle Aeronautical University

  In order to provide a means for testing noise reduction techniques in propellers and fans, a low-speed, low-turbulence, anechoic wind tunnel was designed, fabricated… (more)

Subjects/Keywords: Aerospace Engineering; Propulsion and Power

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APA (6th Edition):

Kaplan, B. J. (1996). The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel. (Masters Thesis). Embry-Riddle Aeronautical University. Retrieved from https://commons.erau.edu/db-theses/91

Chicago Manual of Style (16th Edition):

Kaplan, Brian J. “The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel.” 1996. Masters Thesis, Embry-Riddle Aeronautical University. Accessed January 23, 2020. https://commons.erau.edu/db-theses/91.

MLA Handbook (7th Edition):

Kaplan, Brian J. “The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel.” 1996. Web. 23 Jan 2020.

Vancouver:

Kaplan BJ. The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel. [Internet] [Masters thesis]. Embry-Riddle Aeronautical University; 1996. [cited 2020 Jan 23]. Available from: https://commons.erau.edu/db-theses/91.

Council of Science Editors:

Kaplan BJ. The Design, Fabrication, and Evaluation of a Low-Speed, Low-Turbulence, Anechoic Wind Tunnel. [Masters Thesis]. Embry-Riddle Aeronautical University; 1996. Available from: https://commons.erau.edu/db-theses/91

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