Wind tunnel tests for the Asuka were performed by using a transonic wind tunnel 2 x 2 m from late May to early June. The main purposes of the tests are as follows: to obtain basic aerodynamic data for expanding the flight area to the high-speed side at flight experiments on the Asuka; and to establish technologies necessary for performing tests on a power model in a transonic wind tunnel.
Developments in STOL Aircraft Reported
1987
3 pages
Report
No indication
English
Advanced Propeller Developments for V/STOL Aircraft
SAE Technical Papers | 1965
|Advanced propeller developments for V/STOL aircraft
Engineering Index Backfile | 1965
|