Computational prediction of isolated performance of an axisymmetric nozzle at Mach number 0.90
By: John R. Carlson.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 4506.; NASA technical memorandum -- 4506.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Nozzles.; Fluid dynamics.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 94-0415-M.

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