Aerodynamic drag loss chargeability and its implications in the vehicle design process

1st AIAA, Aircraft, Technology Integration, and Operations Forum

Volumn , Issue , 2001, Pages

  Roth, Bryce ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DESIGN; THERMODYNAMICS;

CHARGEABILITY; DESIGN PROCESS; DESIGN TRADES; DRAG MECHANISMS; SENSITIVITY FACTORS; TOTAL LOSS; VEHICLE DESIGN; VEHICLE MISSION;

AERODYNAMIC DRAG;

EID: 85060946300     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-5236     Document Type: Conference Paper

References (15)

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2. Roth, B.A., Mavris, D.N., Technology Evolution Via Loss Management Models Formulated in terms of Vehicle Weight, Presented at the 59th International Conference on Mass Properties Engineering, St. Louis, June 5-7, 2000, SAWE Paper #3001.
3. Roth, B.A., Mavris, D.N., Minimizing Vehicle Environmental and Economic Cost Via Thermodynamic Work Potential, Presented at the 2001 NSF DMII Grantees Conference, Tampa, FL, January 2001, www.asdl.gatech.edu/pubs.
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10. Crane, C.A., Vance, C.H., Warren, B.L., "F-5E Basic Aerodynamic Drag Data, Vol III: Air Combat Maneuvering Configurations," Northrop Corp., Hawthorne, CA, Report NOR 72-22, Apr. 1972.
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14. Roth, B.A., Mavris, D.N., A Comparison of Thermodynamic Loss Models Suitable for Gas Turbine Propulsion: Theory and Taxonomy," Presented at the 36th Joint Propulsion Conference and Exhibit, Huntsville, AL, July 2000, AIAA2000-3714.
15. Roth, B.A., Mavris, D.N., A Comparison of Thermodynamic Loss Models Applied to the J-79 Turbojet Engine, Presented at the 36th Joint Propulsion Conference and Exhibit, Huntsville, AL, July 2000, AIAA2000-3715.