A comparison of measured and prideicted sphere shock shapes in hypersonic flows with density ratios from 4 to 19/
Main Author: | Miller, Charles G. 1940- |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration, United States. National Aeronautics and Space Administration, Langley Research Center |
Format: | Book |
Language: | English |
Published: |
Washington:
NASA,
1975
|
Series: | NASA technical note
8076 |
Subjects: |
Similar Items
-
Shock shapes on blunt bodies in hypersonic-hypervelocity helium, air and CO2 flows, and calibration results in Langley 6-inch expansion tube/
by: Miller, Charles G. 1940-
Published: (1975) -
Simulation of real-gas effects on pressure distributions for aeroassist flight experiment vehicle and comparison with prediction/
by: Micol, John R.
Published: (1992) -
Special course on Shock-wave/boundary-layer interactions in supersonic and hypersonic flows= Interactions entre ondes de choc et couches limites dans les ecoulements supersoniques et hypersoniques/
Published: (1993) -
Supersonic flow and shock waves/
by: Courant, Richard, 1888-1972
Published: (1977) -
Hypersonic flow theory/
by: Hayes, Wallace Dean
Published: (1966)