Calculations of inviscid flow over shuttle-like vehicles at high angles of attack and comparisons with experimental data/
Main Author: | Weilmuenster, K. James |
---|---|
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: | Hamilton, H. Harris |
Format: | Book |
Language: | English |
Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1983
|
Series: | NASA technical paper
2103 |
Subjects: |
Similar Items
-
Solution of axisymmetric and two-dimensional inviscid flow over blunt bodies by the method of lines/
by: Hamilton, H. Harris
Published: (1978) -
Viscous-inviscid calculations of jet entrainment effects on the subconic flow over nozzle afterbodies/
by: Wilmoth, Richard G.
Published: (1980) -
Calculation of three-dimensional, inviscid supersonic, steady flows/
by: Moretti, Gino
Published: (1982) -
Computational models for the viscous/inviscid analysis of jet aircraft exhaust plumes/
by: Dash, Sanford M.
Published: (1980) -
Experimental design studies and flow visualization of proportional laminar-flow fluidic amplifiers/
by: Hellbaum, R. F.
Published: (1977)