Aerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes /
Lift and drag comparisons were based upon flap settings that would trim the model with the center of gravity placed as far back as possible without producing instability in the airplane under any conditions of level flight
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1933
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
477 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 477 |
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