Stall resistance features of lifting-body airplane configurations

Journal of Aircraft

Volumn 36, Issue 2, 1999, Pages 471-474

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

^a SAN DIEGO STATE UNIVERSITY   (United States)

^b Redwood Aircraft Corporation   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DRAG; FLIGHT DYNAMICS; FUSELAGES; LIFT; VORTEX FLOW;

LIFTING BODY AIRPLANES; STALL RESISTANCE;

TRANSPORT AIRCRAFT;

EID: 0032624704     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2456     Document Type: Article

References (7)

1. Cantilli, E. J., "Saga of the Lifting Body/Flying Wing," Flight Journal, Vol. 1, No. 2, 1996, pp. 56-61.
2. Jane's Encyclopedia of Aviation, Vol. 2, Jane's Information Group, Ltd., Coulsdon, Surrey, UK, 1980, p. 367.
3. Mitchell, K. A., "Burnelli and His Lifting-Body Transports," American Aviation Historical Society Journal, Spring 1997, pp. 2-19.
4. Liebeck, R. H., Page, M. A., and Rawdon, B. K., "Blended-Wing-Body Subsonic Commercial Transport," AIAA Paper 98-0438, Jan. 1998.
5. Hahl, R., and Katz, J., "Lifting-Fuselage/Wing Aircraft Having an Elliptical Forebody," U.S. Patent Appl. 08-642997, May 13, 1996.
6. Raymer, D. P., Aircraft Design: A Conceptual Approach, AIAA Educational Series, AIAA, Washington, DC, 1992, Chap. 12.
7. Katz, J., Byrne, S., and Hahl, R., "Stall Resistance Features of Lifting-Body Airplane Configurations," AIAA Paper 98-0760, Jan. 1998.