Effects of vortex flaps on the low-speed aerodynamic characteristics of an arrow wing/
Main Author: | Yip, Long P. |
---|---|
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, Langley Research Center |
Other Authors: | Murri, Daniel G. |
Format: | Book |
Language: | English |
Published: |
Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1981
|
Series: | NASA technical paper
1914 |
Subjects: |
Similar Items
-
Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps/
by: Yip, Long P.
Published: (1987) -
A common geometric data-base approach for computer-aided manufacturing of wind-tunnel models and theoretical aerodynamic analysis/
by: See, Michael J.
Published: (1983) -
Effect of diffusers, shrouds and mass injection on the starting and operating characteristics of a Mach 5 free jet tunnel/
by: Molloy, John K.
Published: (1971) -
Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)/
by: Arnaiz, Henry H.
Published: (1980) -
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63/
by: Pittman, Jimmy L.
Published: (1980)