Feasibility study of a procedure to detect and warn of low-level wind shear
Barry S. Turkel, Philip A. Kessel, Walter Frost, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, George C. Marshall Space Flight Center
National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981 - Technology & Engineering - 70 pages
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20.6 m/s amplitude aircraft trajectory program airspeed deterioration parameters airspeed deviation parameters airspeed ranged airspeed varied amplitude and frequency amplitude and l/2 angle of attack attack varied B727 Aircraft Performed B727 Using Control combination longitudinal S-shape computer model computer simulation Computer-Simulated Approach Trajectory cosine downbursts Cosine Wave Wind derivative rad Doppler radar Eastern 66 elevator angle Figure fixed gains flight path angle flight path deterioration flight path deviation flight simulator FPDP ft/s full forward glide slope head wind l5.45 m/s amplitude longitudinal S-shape wave longitudinal sine wave longitudinal wave model pilot NASA Ames simulator path deterioration parameters phugoid frequency pilot control pitch angle S-shape and vertical S-Shape Wave Wind shear wave simulated pilot Simulated trajectory Sine Wave Wind tail wind tall wind shear test pilot thrust rate vertical velocity Vref wave amplitude wave of 5.l5 wave of l0.3 wind field wind gradient wind to tail