Viscosity corrections to cone probes in rarefied supersonic flow at a nominal Mach number of 4 / L. Talbot.
Data were obtained for the viscosity corrections to cone probes in supersonic rarefied air flow at a nominal Mach nubmer of 4. The test models consisted of a set of seven geometrically similar 5 degree semivertex angle cones. Additional experiments were made to determine cone surface pressure distri...
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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) ;
3219. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3219
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| Y 3.N 21/5:6/3219 | Available Place a Hold |