Assessment of wind-induced fatigue life for transmission tower-line systems incorporating joint probability distribution of wind speed and direction. [PDF]
Wu S, Liu H, Zhang J, You Y.
europepmc +1 more source
Cascaded guidance, state estimation, and control for depth tracking of underactuated autonomous underwater vehicles. [PDF]
Qu Y, Zhang Q, Xiang X, Yang S, Cai L.
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A simple Schiff base compound as mitigator for the destruction of C-steel in HCl aqueous solutions: practical and theoretical studies. [PDF]
Saleh MGA +7 more
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Analysis of galloping response in ice-coated transmission conductors under wind loads. [PDF]
Wu S, Liu H, Wang Y, Wang Y.
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Surgery of the Anterior Infratemporal Fossa (AITF) and the Pterygopalatine Fossa (PPF) lesions: critical assessment of operative exposure, loss of functioning tissue and morbidity between Extradural Subtemporal Infratemporal Approach (ESITA) and Endonasal Endoscopic Transmaxillary Transpterygoid Approach (EEMP). [PDF]
Jriyasetapong N, Bawornvaraporn U.
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Correction of sonic anemometer angle of attack errors [PDF]
An improved method of correcting for the angle of attack error resulting from the imperfect (co)sine response of ultrasonic anemometers is proposed. The angle of attack, which was calculated as the arctangent of observed wind vectors, contains the angle of attack errors in the vectors themselves, and hence this angle was 'false'.
Taro Nakai +2 more
exaly +6 more sources
High Angle of Attack Aerodynamics
This is a presentation of the methods and results applicable to the study of the complex aerodynamics of a high angle of attack on the part of fighter aircraft. The book contains reference information relevant to three-dimensional separation on viscous flow.
Josef Rom, Rom, Josef
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High Angle of Attack Velocity Vector Rolls
IFAC Proceedings Volumes, 1994Abstract This paper presents the design of a flight control system for performing the velocity vector roll maneuver at high angles of attack. A six degree of freedom model is developed, and the multiple-input multiple-output Quantitative Feedback Theory (QFT) robust control design method is used to treat both the inherent system nonlinearities and ...
K.E. Boyum, M. Pachter, C.H. Houpis
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The author considers the angle-of-attack compensator and the static pressure sensor. A true angle of attack is required to correct static and dynamic pressures. Static pressure is necessary to calculate altitude. Dynamic pressure is necessary to calculate speed. Sensing the angle of attack is crucial to correcting all sensed parameters.
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