Vacuum chamber pressure effects on thrust measurements of low Reynolds number nozzles /

Bibliographic Details

Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Sovey, J. S.
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, [1985]
Series:	NASA technical memorandum ; 86955.
Subjects:	Convergent-divergent nozzles. High vacuum. Separated flow. Thrust measurement.
Online Access:	https://purl.fdlp.gov/GPO/LPS104805