Numerical calculation of scramjet inlet flow
By: Tomiko Ishiguro, Satoru Ogawa and Yasuhiro Wada.
Contributors: Ogawa, Satoru.; Wada, Yasuhiro.; National Aerospace Laboratory (Japan)
Series: Technical report of National Aerospace Laboratory -- TR-1174T
Publisher: National Aerospace Laboratory
Published: 1992
Place of publication: Tokyo, Japan
Number of pages: 29
Subjects: Inlet flow; Supersonic combustion ramjet engines
Notes: Includes bibliographical references: p. 28-29.