Drag minimization for wings in supersonic flow, with various constraints / Max. A. Heaslet and Franklyn B. Fuller.
The minimization of inviscid fluid drag is studied for thin aerodynamic shapes subject to imposed constraints on lift, pitching moment, base area, or volume. The problem is transformed to one of determining a two-dimensional potential flow satisfying either Laplace's or Poisson's equations...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4227. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4227
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| Y 3.N 21/5:6/4227 | Available Place a Hold |