Full-scale investigation of the aerodynamic characteristics of a model employing a sailwing concept /
An investigation has been conducted in the Langley full-scale tunnel to determine the aerodynamic characteristics of a full-scale model employing a sailwing concept and having a wing aspect ratio of 11.5. The wing had a rigid leading-edge spar, rigid root and wing-tip ribs with a trailing-edge stret...
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. : Springfield, VA :
National Aeronautics and Space Administration ; For sale by the Clearinghouse for Federal Scientific and Technical Information,
1967
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| Series: | NASA technical note ;
D-4062 NASA technical note ; D-4062 |
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