Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow
By: by E. R. A. Landers.
Series: Dept. of Supply. Australian Aeronautical Research Committee. Report ACA-70
Publisher: Dept. of Supply, Australian Aeronautical Research Committee
Published: 1900
Place of publication: [Melbourne]
Language: eng
Subjects: Aerodynamics, Supersonic.; Airplanes -- Wings, Triangular.; Pressure.
Notes: Includes bibliographical references.
Table of contents: title: pt. 2. Experimental results for mach numbers 2.00 and 2.58.