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Rocket-model investigation of longitudinal stability and drag characteristics of an airplane configuration have a 60©� delta wing and a high unwept horizontal tail
Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60©� sweptback-wing--indented-body configuration at transonic speeds
Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8
A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body
Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds
Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4
Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing
Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3