Comparison of two procedures for predicting rocket engine nozzle performance
By: Kenneth J. Davidian.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 89814.
Publisher: National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1987
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer.; Rockets (Aeronautics) -- Nozzles.; Rocket engines.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.