Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles/
Main Author: | Yetter, Jeffery A. |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration Scientific and Technical Information Branch, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Joint Institute for Advancement of Flight Sciences, Langley Research Center |
Other Authors: | Leavitt, Laurence D. |
Format: | Book |
Language: | English |
Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1980
|
Series: | NASA technical paper
1771 |
Subjects: |
Similar Items
-
Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model/
by: Capone, Francis J.
Published: (1982) -
Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions/
by: Carson, George T.
Published: (1978) -
Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring/
by: Bare, E. Ann
Published: (1987) -
Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle/
by: Carson, George T.
Published: (1987) -
Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20/
by: Capone, Francis J.
Published: (1977)