The formulation of an influence-coefficient method for determining static aeroelastic effects, and its application to a slender aircraft in symmetric flight at M
2.2
1969
50 S.
graph. Darst.
Buch
Englisch
DDC: | 629.13/008 / 629.1342 / 629.132/362 |
Some static aeroelastic considerations of slender aircraft
Engineering Index Backfile | 1961
|