Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

• 80 Want to read
• 5 Currently reading

Published 1991 by National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, For sale by the National Technical Information Service in Washington, D.C, Springfield, Va .
Written in English

Subjects:

• Convergent-divergent nozzles.,
• Jet vanes.,
• Nozzle geometry.,
• Static tests.,
• Static thrust.,
• Thrust vector control.,
• Yaw.,
• Jet nozzles -- Testing.,
• Blades.,
• Yawing (Aerodynamics),
• Airplanes -- Motors -- Thrust.

---

Edition Notes

Statement	Robert J. Foley, Odis C. Pendergraft, Jr.
Series	NASA technical paper -- 3085.
Contributions	Pendergraft, Odis C., Langley Research Center.
The Physical Object
Format	Microform
Pagination	iii, 77 p.
Number of Pages	77
ID Numbers
Open Library	OL17723834M

---