Wing morphing for quiet supersonic jet performance - Variable geometry design challenges for business jet utilization

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 14923-14931

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

^a GULFSTREAM AEROSPACE CORPORATION   (United States)

^b M/S C 215 ^*

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC EFFICIENCY; STRUCTURAL MORPHING; SUBSONIC BUSINESS JETS;

AIRPORTS; JET AIRCRAFT; JETS; SUBSONIC FLOW; SUPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; WINGS;

SUPERSONIC FLOW;

EID: 30744478432     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Phan, Leon L., Yamaoka, Yohei, Mavris, Dimitri N., "Implementation and Benefits of Variable Geometry Wings for a Supersonic Business Jet", AIAA 2003-6812, American Institute of Aeronautics and Astronautics, 2003.
2. Harvey, J.W., "Structural Considerations for Variable Sweep Wings", SAE 670881, Society of Automotive Engineers, 1967.
3. Bhatia, Kumar G, Werheimer, Jiri, "Aeroelastic Challenges for a High Speed Civil Transport", AIAA-93-1478-CP, American Institute of Aeronautics and Astronautics, 1993.
4. Beissner, F.L., Lovell, W.A., Robins, A.W. and Swanson, E.E., "Application of Near-Term Technology to a Mach 2.0 Variable-Sweep-Wing, Supersonic-Cruise Executive Jet", NASA-CR-172321, 1984.
5. Paget, F.M., "Mechanical Aspects of Variable Sweep Wings", SAE 670882, Society of Automotive Engineers, 1967.
6. Newell, G.C. and Marsh, F.E.,"Reliability of the SST Wing-Sweep Actuation System", SAE 670884, Society of Automotive Engineers, 1967.
7. Alexander, Marvin M., "Structural Problems Associated with Variable Geometry", World Aerospace Systems, March 1966.
8. Foreman, C.R., "The Design and Testing of a Wing Pivot Joint for Variable Geometry Aircraft", Vought Aeronautics Division, LTV Aerospace Corp., Dallas, Texas, 1967.