Aerodynamic and flow visualization studies of variations in the geometry of irregular planform wings at a mach number of 20.3/
Main Author: | Stone, David R. |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center |
Other Authors: | Spencer, Bernard |
Format: | Book |
Language: | English |
Published: |
Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Office,
1974
|
Series: | NASA technical note
D-7650 |
Subjects: |
Similar Items
-
Hypersonic aerodynamics and entry-maneuver : aerothermodynamic interactions for two lifting entry vehicles /
by: Arrington, James P.
Published: (1972) -
Viking entry vehicle aerodynamics at M=2 in air and some preliminary test data for flight in CO_2 at M=11/
by: Sammonds, Robert I.
Published: (1975) -
Wind-tunnel investigation of the aerodynamic pressures on the Apollo launch escape vehicle configuration/
by: Moseley, William C.
Published: (1970) -
Wind-tunnel investigation of the aerodynamic pressures on the Apollo command module configuration/
by: Moseley, William C.
Published: (1969) -
Dynamics of atmospheric re-entry
by: Regan, Frank J.
Published: (1993)