This is the second report giving the results obtained in the NACA 20-foot wind tunnel on the drag due to landing gears. The present report gives the results of tests of nonretractable and partly retractable landing gears intended for heavier low-wing monoplanes of the transport and bomber type.
The Drag of Airplane Wheels, Wheel Fairings, and Landing Gears II : Nonretractable and Partly Retractable Landing Gears
1936-01-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1935
|Engineering Index Backfile | 1935
|Drag of airplane wheels, wheel fairings, and landing gears
Engineering Index Backfile | 1934
|