Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow
Subtitle: part 1-theoretical results for the wing thickness case
By: by Y. Y. Chan and L. M. Sheppard.
Contributors: Sheppard, L. M., joint author.
Series: Dept. of Supply. Australian Aeronautical Research Committee. Report ACA-69
Publisher: Dept. of Supply, Australian Aeronautical Research Committee
Published: 1966
Place of publication: [Melbourne]
Language: eng
Number of pages: 82
Subjects: Airplanes -- Wings, Triangular.; Aerodynamics, Supersonic.
Notes: Includes bibliographical references.