Application of an aerodynamic analysis method including attainable thrust estimates to low speed leading-edge flap design for supersonic cruise vehicles
By: Harry W. Carlson.
Contributors: Langley Research Center.
Series: NASA contractor report -- 165843.; NASA contractor report -- NASA CR-165843.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1985
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Aerodynamics.; Airplanes -- Wings.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1985. 1 microfiche.