There are three lateral dynamic attitudes, delineated by rolling, yawing, and sideslipping. It is possible to solve for the pressures on the rolling wing by quasi-steady analysis. This approach is, however, inapplicable for the yawing or sideslipping wing, and it is with the latter two cases that this paper deals.
Institute of the Aeronautical Sciences Annual Meeting
Summaries of Papers Presented to the 23rd Annual General Meeting Held in New York on January 24–27, 1955
Aircraft Engineering and Aerospace Technology ; 27 , 4 ; 117-124
1955-04-01
8 pages
Article (Journal)
Electronic Resource
English
Annual Meeting of Institute of Aeronautical Sciences
Engineering Index Backfile | 1949
Annual Meeting of Institute of Aeronautical Sciences
Engineering Index Backfile | 1947
|Tenth annual meeting of institute of aeronautical sciences
Engineering Index Backfile | 1942
|Ninth annual meeting of Institute of Aeronautical Sciences
Engineering Index Backfile | 1941
The Annual Meeting of the Institute of Aeronautical Sciences
Emerald Group Publishing | 1946