Schlieren photographs and internal pressure distributions for three-dimensional sidewall-compression scramjet inlets at a Mach number of 6 in CF4
By: Scott D. Holland.
Contributors: Langley Research Center
Publisher: Langley Research Center
Published: 1993
Place of publication: Hampton, Va
Number of pages: 140
Subjects: Inlets; Supersonic combustion ramjet engines
Notes: Includes bibliographical references: p. 6.