A modificiation to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack
By: Harry W. Carlson, Langley Research Center
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA technical paper ; 1406
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; for sale by the National Technical Information Service
Published: 1979
Place of publication: Washington; Springfield, Va
Language: eng
Number of pages: 36
Subjects: Aerodynamic load; System analysis; Aerodynamics, Supersonic
Notes: February 1979

Includes bibliographical references