Study of Exit Phase of Flight of a Very High Altitude Hypersonic Airplane by Means of a Pilot-controlled Analog Computer
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Sherman, Windsor L↗
Engineering topics
Sherman, Windsor L
Publications and source records attributed to Sherman, Windsor L.
Analog computer study of some filtering, command-computer, and automatic-pilot problems connected with the attack phase of the automatically controlled supersonic interceptor
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Sherman, Windsor L↗
Theoretical investigation of the attack phase of an automatic interceptor system at supersonic speeds with particular attention to aerodynamic and dynamic representation of the interceptor
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Sherman, Windsor L↗
Simulator studies of the attack phase of an automatically controlled interceptor
The attack phase of the automatically controlled interceptor is studied in two parts. Part I is a limited simulation conducted to specify the lateral and longitudinal control systems for an automatic interceptor. The results are presented as Nyquist plots and time histories of the airplane variables. Part II uses the control systems developed in Part I, together with a dynamically perfect guidance system, to study the effect of the nonlinear terms in the complete equations of motion and nonlinear aerodynamics on the airplane response. The results are presented as time histories of the airplane and control surface motions.
CONTROL, LONGITUDINAL↗
A theoretical investigation of a compensating network with application to roll control systems for automatic interceptors
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Sherman, Windsor L↗
Theoretical calculations of the effects of finite sideslip at supersonic speeds on the span loading and rolling moment for families of thin sweptback tapered wings at an angle of attack
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WINGS, COMPLETE - ASPECT RATIO↗
Theoretical calculation of the pressure distribution, span loading, and rolling moment due to sideslip at supersonic speeds for thin sweptback tapered wings with supersonic trailing edges and wing tips parallel to the axis of wing symmetry
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Margolis, Kenneth↗