Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰
By: Laurence D. Leavitt.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2391.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch
Published: 1985
Place of publication: [Washington, D.C.]
Language: eng
Format: Microform
Subjects: Jet nozzles -- Testing.
Notes: "February 1985"--Cover.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1985] 1 microfiche.