Effect of fin passage length on optimization of cylinder head cooling fins/
Main Author: | Siegel, Robert, 1927- |
---|---|
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, Lewis Research Center |
Other Authors: | Graham, Robert W. |
Format: | Book |
Language: | English |
Published: |
Washington:
National Aeronautics and Space Administration, Scientific and Technical Information Office,
1977
|
Series: | NASA technical paper
1054 |
Subjects: |
Similar Items
-
Actively cooled plate fin sandwich structural panels for hypersonic aircraft/
by: Smith, L. M.
Published: (1979) -
Effects of visual and motion simulation cueing systems on pilot performance during takeoffs with engine failures/
by: Parris, Benton L.
Published: (1978) -
Transportation and power/
by: Johnson, William Harding, 1895-
Published: (1944) -
Technical evaluation report on the 49th (B) Propulsion and Energetics Panel specialists' meeting on power plant reliability/
by: Sallee, G. P.
Published: (1977) -
Evaluation of various thrust calculation techniques on an F404 engine/
by: Ray, Ronald J.
Published: (1990)