The Ames 10- by 14-inch supersonic wind tunnel / A.J. Eggers, Jr. and George J. Nothwang.
The Ames 10- by 14-inch supersonic wind tunnel is described and pertinent features of the design and operation of the facility are included. The wind tunnel is capable of continuous operation at Mach numbers from 2.7 to 6.3 and Reynolds numbers from 1 million to 11 million per foot. Results of surve...
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Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3095. |
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PASCAL Offsite
Call Number: |
Y 3.N 21/5:6/3095
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Y 3.N 21/5:6/3095 | Available Place a Hold |