An approximate theoretical method for modeling the static thrust performance of non-axisymmetric two-dimensional convergent-divergent nozzles
By: Craig A. Hunter.
Contributors: Langley Research Center.
Series: NASA contractor report -- 195050.; NASA contractor report -- NASA CR-195050.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer equations.; Compressible flow.; Convergent-divergent nozzles.; Mathematical models.; Nozzle design.; Nozzle efficiency.; Nozzle flow.; Performance prediction.; Static thrust.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0479-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.