Research Catalog

Details

Additional authors

1. Pendergraft, Odis C.
2. Langley Research Center.

Description

1. iii, 77 p. : ill.; 28 cm.

Series statement

1. NASA technical paper ; 3085

Subject

1. Convergent-divergent nozzles
2. Jet vanes
3. Nozzle geometry
4. Static tests
5. Static thrust
6. Thrust vector control
7. Yaw
8. Jet nozzles > Testing
9. Blades
10. Yawing (Aerodynamics)
11. Airplanes > Motors > Thrust

Call number

1. GPO Microfiche NAS 1.60:3085

Note

1. Prepared at Langley Research Center.

Bibliography (note)

1. Bibliography: p. 11.

Reproduction (note)

1. Microfiche.

Author

1. Foley, Robert J.

Title

1. Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes [microform] / Robert J. Foley, Odis C. Pendergraft, Jr.

Imprint

1. Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, [1991]

Series

1. NASA technical paper ; 3085

Bibliography

1. Bibliography: p. 11.

Reproduction

1. Microfiche. Washington, D.C. : National Aeronautics and Space Administration, 1991. 2 microfiche.

Added author

1. Pendergraft, Odis C.
2. Langley Research Center.

Gpo item no.

1. 0830-H-15 (MF)

Sudoc no.

1. NAS 1.60:3085

Research call number

1. GPO Microfiche NAS 1.60:3085