Effect of lag of sidewash on the vertical-tail contribution to oscillatory damping in yaw of airplane models / Lewis R. Fisher and Herman S. Fletcher.
Two models were tested for which the rate of change of sidewash with angle of sideslip could be varied. For the first model, this effect was obtained by mounting auxiliary vertical fins on the fuselage at the assumed center of gravity; for the second model, the change in the gradient of the sidewash...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1955]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3356. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3356
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| Y 3.N 21/5:6/3356 | Available Place a Hold |