Results 91 to 100 of about 1,277,064 (238)
Implications of control technology on aircraft design [PDF]
, 1984 New controls technologies are now available for implementation with aircraft systems. Many aircraft with state of the art technology in the fields of aerodynamics, structures, and propulsion require extensive augmentation merely for safety of flight ...
Arbuckle, P. D., Sliwak, S. M.
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, 1990 A means for extracting rotational energy from the vortex created at aircraft wing tips which consists of a turbine with blades located in the crossflow of the vortex and attached downstream of the wingtip. The turbine has blades attached to a core.
Patterson, James C., Jr.
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Application of refractory high entropy alloys on aero-engines
Journal of Aeronautical Materials, 2019 High strength and low density are the basic requirements for the materials used in the aeronautical field, the engine materials need high temperatures resistance more severely.
WEI Yaoguang +4 more
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Development of the Kalman filter modification for the measuring complex of the aircraft for carrier landing [PDF]
, 2019 Lu Wang
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Aircraft control position indicator [PDF]
, 1987 An aircraft control position indicator was provided that displayed the degree of deflection of the primary flight control surfaces and the manner in which the aircraft responded.
Dennis, Dale V.
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Peculiarities of bead shape regulation in single-layer microplasma surfacing on edges of aircraft gas turbine engine blades [PDF]
, 2016 P. D. Zhemanyuk +4 more
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Springer Handbook of Atmospheric Measurements, 2021 J. Bange, J. Reuder, A. Platis
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A study of noise metric and tone correction accuracy [PDF]
Methods currently used to measure human response to aircraft flyover noise were investigated. Response to high level aircraft noise usually experienced outdoors was obtained.
Mabry, J. E., Sullivan, B. M.
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Rotatable non-circular forebody flow controller [PDF]
, 1991 The invention is a rotatable, non-circular forebody flow controller. The apparatus comprises a small geometric device located at a nose of a forebody of an aircraft and a non-circular cross-sectional area that extends toward the apex of the aircraft. The
Moskovitz, Cary A.
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Study on aerodynamic characteristics of tilting wing unmanned aerial vehicle in transition state
Hangkong gongcheng jinzhanIn response to the problem of the continuous tilting transition process of the configuration of unmanned aerial vehicle with complex and unsteady aerodynamic characteristics, the real blade is replaced with a virtual propeller disk model, the rotor flow ...
MA Kai +4 more
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