Calibration of HYPULSE for hypervelocity air flows corresponding to flight mach numbers 13.4, 15, and 17
By: John Calleja and Jose Tamagno.
Contributors: Tamagno, Jose.; Langley Research Center.
Series: NASA contractor report -- 191578.; NASA contractor report -- NASA CR-191578.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1993
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Shock tubes.; Shock waves.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0441-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.