The linearized subsonic flow about symmetrical nonlifting wing-body combinations / John B. McDevitt.
Methods are presented for determining the linearized subsonic flow about symmetrical, nonlifting wing-body combinations. The wing is represented by a suitable planar distribution of elementary sources in accordance with the usual assumptions of linearized, thin-airfoil theory. The required boundary...
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Format: | Government Document Book |
Language: | English |
Published: |
Washington :
National Advisory Committee for Aeronautics,
[1957]
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3964. |
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Call Number: |
Y 3.N 21/5:6/3964
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Y 3.N 21/5:6/3964 | Available Place a Hold |