Publication Date:
2019-06-28
Description:
The tests were conducted at Mach numbers from 0.40 to 0.90, at angles of attack up to 45 deg for the lower Mach numbers, and at angles of sideslip up to 15 deg. The model variations under study included adding a canard surface and deflecting horizontal tails, ailerons, and rudders.
Keywords:
AERODYNAMICS
Type:
NASA-TM-83171
,
L-14433
Format:
application/pdf