Publication Date:
2019-07-12
Description:
Wind-tunnel tests of a full-scale model of the Republic XF-91 airplane having swept-back wings and a vee tail were conducted to determine both the stability and control characteristics of the model longitudinally, laterally, and directionally. Configurations of the model were investigated involving such variables as external fuel tanks, a landing gear, trailing-edge flaps, leading-edge slats, and a range of wing incidences and tail incidences.
Keywords:
Fluid Mechanics and Thermodynamics
Type:
NACA-RM-SA9C04
Format:
application/pdf