Measured and predicted shock shapes for AFE configuration at mach 6 in air and in FD₄
By: William L. Wells, Alan M. Franks.
Contributors: Franks, Alan M.; Langley Research Center.
Series: NASA technical memorandum -- 100660.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1988
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Air.; Carbon tetrafluoride.; Orbit transfer vehicles.; Prediction analysis techniques.; Shock.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990] 1 microfiche.