Flow studies on flat-plate delta wings at supersonic speed / William H. Michael, Jr.
An experimental study has been made to investigate some aspects of the nature of the flow around delta wings. Vapor-screen, pressure-distribution, and ink-flow studies were made at a Mach number of 1.9 on a series of semispan delta-wing models with slender wedge airfoil sections and very sharp leadi...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3472. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3472
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| Y 3.N 21/5:6/3472 | Available Place a Hold |