Spin-tunnel investigation to determine the effectiveness of a rocket for spin recovery / Anshal I. Neihouse.
Consideration is given to use of a jet-reaction device for emergency spin recovery. Brief tests made in the Langley 20-foot free-spinning tunnel on a dynamic scale model with a reaction rocket fired rearward from the inboard wing tip (right wing tip in a right spin) indicated that such a device woul...
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| Other title: | Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1866. |
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Internet
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| Call Number: |
Y 3.N 21/5:6/1866
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| Y 3.N 21/5:6/1866 | Available Place a Hold |