Stall resistance features of lifting-body airplane configurations

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Katz, Joseph ^a   Byrne, Shaun ^a   Hahl, Robert ^b  

^a UTC Aerospace Systems   (United States)

^b Redwood Aircraft Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AERODYNAMIC STALLING; AEROSPACE ENGINEERING; AIRCRAFT; AIRCRAFT MODELS; ANGLE OF ATTACK; FUSELAGES; GEOMETRY; LIFT; LIFT DRAG RATIO; TRACKING (POSITION); WIND TUNNELS;

AERODYNAMIC EFFECT; ANGLES OF ATTACK; HIGH ANGLE OF ATTACK AERODYNAMICS; HIGH-EFFICIENCY; LIFTING BODIES; LOW-SPEED WIND TUNNEL; PERFORMANCE CURVE; PITCHING MOMENTS;

AERODYNAMICS;

EID: 84983167765     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Cantilli E., "Saga of the Lifting Body/Flying Wing," Flight, pp. 56-61, Fall 1996.
2. Jane's Encyclopedia of Aviation, Vol. 2, p. 367, 1980.
3. Mitchell, K. A., "Bumelli and his Lifting-Body Transports," American Aviation Historical Society Journal, pp. 2-19, Spring 1997.
4. Kroo, I., McMasters, J., and Smith, S.C., "Highly Nonplanar Lifting Systems," NASA CP 10184, pp. 331-370, Feb. 1996.
5. Hahl R., and Katz, J, "Lifting-Fuselage/Wing Aircraft having an Elliptical Forebody," U.S. patent appl. 08642997, May 13, 96.
6. Raymer D. P., "Aircraft Design: A Conceptual Approach," AIAA Educational Series, 1992.
7. Jones R. T. "Properties of Low-Aspect-Ratio Pointed Wings at Speeds Below and Above the Speed of Sound," NACA rep. 835, May 1945.