Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
Main Author: | Carson, George T |
---|---|
Corporate Author: | United States National Aeronautics and Space Administration Scientific and Technical Information Division |
Other Authors: | Capone, Francis J |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. : [Springfield, Va. :
National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service],
1991
|
Series: | NASA technical memorandum
4237 |
Subjects: |
Similar Items
-
Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability
by: Wing, David J, et al.
Published: (1997) -
Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° /
by: Berrier, Bobby L, et al.
Published: (1984) -
Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60 ̊ /
by: Leavitt, Laurence D., et al.
Published: (1985) -
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
by: Mason, Mary L
Published: (1985) -
Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
by: Re, Richard J
Published: (1986)