Measurements of the pressure distribution on the horizontal-tail surface of a typical propeller-driven pursuit airplane in flight 3, Tail loads in abrupt pull-up push-down maneuvers /
The total horizontal-tail load and root bending-moment increments calculated by the use of existing rational procedures are compared with the experimental values obtained in abrupt pull-up push-down maneuvers obtained on a representative pursuit-type airplane. The computed loads were determined for...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1948
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1539 |
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| Call Number: |
NACA TN 1539 |
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