Delta wings with shock-free cross flow
By: S.S. Sritharan.
Contributors: Institute for Computer Applications in Science and Engineering.; Langley Research Center.
Series: NASA contractor report -- 172297.; NASA contractor report -- NASA CR-172297.
Publisher: institute for Computer Applications in Science and Engineering, NASA Langley Research Center
Published: 1984
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Wings, Triangular.; Cross-flow (Aerodynamics); Camber.; Cross flow.; Delta wings.; Potential flow.; Shock waves.; Supersonic airfoils.
Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 1 microfiche.