Wind tunnel tests on slotted flaps on a low wing monoplane : flap angle 0 o to 90 o
degrees
1936
14 S.
Sonstige
Englisch
RVK: | ZO 7000 |
Wind tunnel tests on high wing monoplane with running propeller
Engineering Index Backfile | 1936
|Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle
Engineering Index Backfile | 1936
|