Morphing concept for quiet supersonic jet boom mitigation

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 3783-3792

  Simmons III, Frank ^a,b,c   Freund, Donald ^a,b,c  

^a GULFSTREAM AEROSPACE CORPORATION   (United States)

^b MS C 215 ^*

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

QUIET SUPERSONIC JET (QSJ); RETRACTION MECHANISM; SONIC BOOMS;

AERODYNAMICS; AIRCRAFT; FUSELAGES; JETS; SHOCK WAVES; TELESCOPES;

ACOUSTIC WAVES;

EID: 30744479473     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Howe, D.C., "Improved Sonic Boom Minimization with Extendable Nose Spike", Reno, NV, AIAA 2005-1014.
2. Code of Federal Regulations, Title 14, Part 25, Section 25.473, "Landing Load Conditions and Assumptions".
3. Simmons, F. and Freund, D.,"Wing Morphing for Quiet Supersonic Jet Performance", Reno, NV, AIAA paper 2005-1017.
4. Richter, B. J., "Structural Evaluation of Deployable Aerodynamic Spike Booms", NASA Kennedy Space Center 9th Aerospace Mech. Symposium, p 31-43, Aug 1, 1976.
5. EDSU paper 89008, "Normal-Force-Curve And Pitching-Moment-Curve Slopes Of Forebody-Cylinder Combinations At Zero Angle Of Attack For Mach Numbers Up To 5", April 1989.
6. Code of Federal Regulations, Title 14, Part 25, Section 25.1309, "Equipment, Systems, and Installations".