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 Astronautics and Aeronautics Mar 1966 v 4 n 3 p 64-7)
Airplane spinning
NASA SP
NASA Special Publication ; Publ 83
1965
9 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
NTRS | 1965
|Engineering Index Backfile | 1966
|NTRS | 1966
|Airplane spinning characteristics
Engineering Index Backfile | 1928
|Engineering Index Backfile | 1928
|