A flight study of the effects of noise filtering in the attack display on the pilot's tracking performance
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Turner, Howard L↗
Engineering topics
Turner, Howard L
Publications and source records attributed to Turner, Howard L.
Tracking Performance of a Swept-wing Fighter with a Director-type Radar Fire-control System and Scope Presentation
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Turner, Howard L↗
A Flight and Analog Computer Study of Some Stabilization and Command Networks for an Automatically Controlled Interceptor During the Final Attack Phase
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Turner, Howard L↗
Flight Testing by Radio Remote Control-flight Evaluation of a Beep-control System
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Turner, Howard L↗
Flight testing by radio remote control flight evaluation of a beep control system
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Turner, Howard L↗
Measurement of the Moments of Inertia of an Airplane by a Simplified Method
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PENDULUM APPARATUS - NACA↗
A comparison with flight data of vertical-tail loads in various maneuvers estimated from sideslip angles and rudder deflections
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Turner, Howard L↗
Sideslip angles and vertical-tail loads in rolling pull-out maneuvers.
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White, Maurice D↗
Pressure Lag in Tubing Used in Flight Research
Tests described in this report were undertaken to obtain a quantitative measure of the pressure lag in typical pressure-tubing systems used by the Ames Aeronautical Laboratory in flight research investigations. Lag measurements were made with both single-direction and oscillating pressure changes. Single-direction pressure changes were investigated to determine if the lag in orifice-pressure lines and in the research airspeed and altitude measuring systems of pursuit-type airplane undergoing flight tests was sufficient to cause an appreciable error in the record of a sudden pressure change. Oscillating pressure changes were investigated with particular reference to the accuracy of pressure peaks in pressure-distribution measurements during the time of buffeting conditions as found in stalls. (author)
Turner, Howard L↗