Summary on spinning is presented to point out state of art and most important parameters, and to show effects of parameters on spin and spin-recovery characteristics; principal factors in spinning are mass distribution, which is by far most important single parameter, and tail design, which is important for conditions of zero or near-zero loading; by knowing mass distribution and tail design, it is possible to predict whether airplane has satisfactory spin-recovery characteristics. (See also NASA SP-83 May 10-12 1965 p 265-73)
Airplane spinning
Astronautics Aeronautics
Astronautics and Aeronautics ; 4 , n 3
1966
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
NTRS | 1965
|Engineering Index Backfile | 1965
|NTRS | 1966
|Airplane spinning characteristics
Engineering Index Backfile | 1928
|Engineering Index Backfile | 1928
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