Flight Tests of an Airplane Model with a 62 Degree Swept-back Wing in the Langley Free-flight Tunnel
1947-05-01
Miscellaneous
No indication
English
WINGS, SWEPTBACK - STABILITY , STALLING - SWEPTBACK WINGS , STABILITY & CONTROL, DYNAMIC , GENESE 33 - CHAR & MOMENTS , AIRFOILS - NACA 0009 TAIL SURFACE , AIRFOILS - RHODE ST , OSCILLATIONS, LATERAL , LIFT & DRAG - WINGS, SWEPTBACK , ROLLING MOMENTS - EFFECTS OF SIDESLIPPING , TAIL SURFACES - POSITION , WINGS - DIHEDRAL
Flight tests of airplane model with 62° swept-back wing in Langley free-flight tunnel
Engineering Index Backfile | 1947
|Flight tests of airplane model with 42° swept-back wing in Langley free-plight tunnel
Engineering Index Backfile | 1947
|