An investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30 degree swepptback wing at transonic speeds
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| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce],
[1961]
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| Series: | NASA technical note ;
D-620 |
| Subjects: |