Wind tunnel tests on aspect ratio 2.17 delta wing model with midchord boundary layer control flaps
Large-scale wind-tunnel tests on an aspect ratio 2.17 delta-wing model equipped with midchord boundary-layer-control flaps
01.12.1964
Sonstige
Keine Angabe
Englisch
Engineering Index Backfile | 1959
|Engineering Index Backfile | 1959
|