Conceptual design of a sonic boom constrained supersonic business aircraft

AIAA Paper

Volumn , Issue , 2004, Pages 8099-8109

  Aronstein, David C ^a   Schueler, Kurt L ^a  

^a RAYTHEON COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

SONIC BOOM; SONIC BOOM SIGNATURES; SUPERSONIC AIRCRAFTS; SUPERSONIC FLIGHT;

ACOUSTIC NOISE; AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; DRAG; FUSELAGES; PROCESS ENGINEERING; PRODUCT DESIGN; WINGS;

AEROSPACE ENGINEERING;

EID: 2942722685     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (18)

1. Blateau, V., et al., "Beyond the Barrier: The Case for A Practical Small Supersonic Transport", Massachusetts Institute of Technology, 16.899 Aircraft Systems Engineering Design Report, May, 2001.
2. Mack, R. and Haglund, G., "A Practical Low-Boom Overpressure Signature Based on Minimum Sonic Boom Theory," High-Speed Research: Sonic Boom Volume II, NASA Conference Publication 3173, 1992.
3. Saiyed, Naseem, Initial Development of Technology Goals and Roadmaps for 12 Notional Air Vehicles, Vehicle Systems Program, NASA Headquarters, Washington, D.C., April 2003.
4. Darden, C., "Sonic Boom Minimization With Nose-Bluntness Relaxation" NASA TP-1348, 1979.
5. Coen, P., Development of a Computer Technique for the Prediction of Transport Aircraft Flight Profile Sonic Boom Signatures, George Washington University Master's Thesis, 1991.
6. Carlson, H., et al., "Guides to AERO2S and WINGDES Computer Codes for Prediction and Minimization of Drag Due to Lift," NASA Technical Paper 3637. 1997.
7. Miranda, L., Elliott, R. and Baker, W., "A Generalized Vortex Lattice Method for Subsonic and Supersonic Row Applications," NASA Contractor Report 2865. 1977.
8. Harris, R. Jr., "An Analysis and Correlation of Aircraft Wave Drag," NASA TM X-947. 1964.
9. McCullers, L., Flight Optimization System Release 6.01 User's Guide, NASA Langley Research Center, Hampton, VA, 2002.
10. Whitham, G.B., "The Flow Pattern of a Supersonic Projectile," Communications on Pure and Applied Mathematics, v.V, n.3, August, 1952.
11. Walkden, F., "The Shock Pattern of a Wing-Body Combination, Far from the Flight Path," Aeronautical Quaterly, v.IX, pt. 2, May, 1958.
12. Alonso, J.J. and Kroo, M.I., "Advanced Algorithms for Design and Optimization of Quiet Supersonic Platforms," Proceedings of the 40th AIAA Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, January 14-17, 2002, Reno, NV.
13. Hayes, W.D., Haefeli, R.C., and Kulsrud, H.E., "Sonic Boom Propagation in a Stratified Atmosphere, with Computer Program," NASA CR-1299, 1969.
14. Seebass, R. and George, A.R., "Sonic Boom Minimization" Journal of the Acoustical Society of America, v.51, n. 2, pt. 3, February, 1972.
15. Pawlowski, J., and Graham, D., Overview of the Shaped Sonic Boom Demonstrator Program, Abstract for the Society of Automotive Engineers, General Aviation Technology Conference & Exhibition, Wichita, Kansas, to be held in April 2004.
16. Torenbeek, Egbert, Synthesis of Subsonic Airplane Design, Delft University Press, Delft, Holland, 1982.
17. Roskam, Jan, Airplane Design, Part V: Component Weight Estimation, Roskam Aviation and Engineering Corporation, Ottawa, Kansas, 1989.
18. rd Edition, American Institute of Aeronautics & Astronautics, Reston, VA, 1999.