Investigation of Axisymmetric and nonaxisymmetric nozzels installed on a 0.10-scale F-18 protype airplane model/
Main Author: | Capone, Francis J. |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Langley Research Center |
Other Authors: | Berrier, Bobby L. |
Format: | Book |
Language: | English |
Published: |
Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Office,
1980
|
Series: | NASA technical paper
1638 |
Subjects: |
Similar Items
-
Utilization of a fixed-base simulator to study the stall and spin characteristics of fighter airplanes/
Published: (1971) -
Multiaxis control power from thrust vectoring for a supersonic fighter aircraft model at Mach 0.20 to 2.47/
by: Capone, Francis J.
Published: (1987) -
Control-system techniques for improved departyre/spin resistance for fighter aircraft/
by: Nguyen, Luat T.
Published: (1980) -
Summary of flight tests to determine the spin and controllability characteristics of a remotely piloted, large-scale (3/8) fighter airplane model/
by: Holleman, Euclid C.
Published: (1976) -
Pressures measured in flight on the aft fuselage and external nozzle of a twin-jet fighter/
Published: (1983)