Effects of vertical fins near the nose of the fuselage on the directional and damping-in-yaw stability derivatives of an airplane model under steady-state and oscillatory conditions / M.J. Queijo and Evalyn G. Wells.
A wind-tunnel investigation has been made at low speed to determine the effects of vertical fins placed ahead of the vertical tail on the directional stability and damping-in-yaw characteristics of a swept-wing model under steady-state oscillatory conditions. Various sizes of fins were used above an...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3814. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3814
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| Y 3.N 21/5:6/3814 | Available Place a Hold |