Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6/
Main Author: | Penland, Jim A. |
---|---|
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: | Marcum, Don C. |
Format: | Book |
Language: | English |
Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Office,
1987
|
Series: | NASA technical paper
2728 |
Subjects: |
Similar Items
-
Reynolds number effects in transonic flow/
by: Elsenaar, A.
Published: (1988) -
An experimental and analytical investigation of the effect on isolated boattail drag of varying Reynolds number up to 130 x 106/
by: Reubush, David E.
Published: (1976) -
Aerodynamic testing at high Reynolds numbers and transonic speeds/
by: Kuchemann, Dietrich, 1911-1976
Published: (1971) -
Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations/
by: Reubush, David E.
Published: (1976) -
A review of some Reynolds number effects related to bodies at high angles of attack/
by: Polhamus, Edward C., 1948-
Published: (1984)