Normal- and oblique-shock flow parameters in equilibrium air including attached-shock solutions for surfaces at angles of attack, sweep, and dihedral
By: James L. Huntand Sue W. Souders ; prepared by Langley Research Center.
Contributors: Souders, Sue W.; Langley Research Center.
Series: NASA SP -- 3093
Publisher: Scientific and Technical Information Office, National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1975
Place of publication: Washington; Springfield, Va
Language: eng
Number of pages: 154
Subjects: Aerodynamics, Hypersonic -- Tables.; Angle of attack (Aerodynamics)
Notes: Includes bibliographical references.