Publication Date:
2019-07-10
Description:
An investigation has been made in the Langley spin tunnel to determine the spin and spin-recovery characteristics of the F-111A airplane in the symmetric and asymmetric stores loading conditions. Tests were also made with the model in the clean condition to determine whether the spin-recovery characteristics could be improved by the use of supplementary devices.
Keywords:
Aerodynamics
Type:
NASA-TM-SX-2970
Format:
application/pdf