Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row/
Main Author: | Farrell, Charles A. |
---|---|
Corporate Authors: | United States National Aeronautics and Space Administration Scientific and Technical Information Branch, Lewis Research Center, United States. National Aeronautics and Space Administration., Scientific and Technical Information Branch |
Format: | Book |
Language: | English |
Published: |
Washington, D.C.:
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
1982
|
Series: | NASA technical paper
2030 |
Subjects: |
Similar Items
-
Improved method for calculating transonic velocities on blade-to-blade stream surfaces of a turbomachine/
by: Wood, Jerry R.
Published: (1981) -
Fluid dynamics for the study of transonic flow
by: Ramm, Heinrich J.
Published: (1990) -
Computation of transonic boattail flow with separation/
by: Wilmoth, Richard G.
Published: (1977) -
Damping seals for turbomachinery/
by: Von Pragenau, George L.
Published: (1982) -
The status of analytical preparation for two-dimensional testing at high transonic speeds in the University of Southampton transonic self-streamlining wind tunnel/
by: Lewis, M. C.
Published: (1984)