Comparison of Airspeed Calibrations Evaluated by the Accelerometer and Radar Methods PDF Download
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Author: Lindsay J. Lina
Publisher:
ISBN:
Category : Accelerometers
Languages : en
Pages : 24
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Book Description
Airspeed calibration of the pitot-static installation on a jet fighter airplane was made to compare the accelerometer method of determining the static-pressure error with the radar method. The tests included shallow dives up to a Mach number of about 0.80 with pull-ups of about 4, 3, and 2g normal acceleration. The results of the test indicated that, for vertical plane maneuvers, the accelerometer method may be used as an alternate to the radar method.
Author: Lindsay J. Lina
Publisher:
ISBN:
Category : Accelerometers
Languages : en
Pages : 24
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Book Description
Airspeed calibration of the pitot-static installation on a jet fighter airplane was made to compare the accelerometer method of determining the static-pressure error with the radar method. The tests included shallow dives up to a Mach number of about 0.80 with pull-ups of about 4, 3, and 2g normal acceleration. The results of the test indicated that, for vertical plane maneuvers, the accelerometer method may be used as an alternate to the radar method.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 862
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Book Description
Author: Carl Kaplan
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 252
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 36
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162
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Book Description
Author: Paul T. Hacker
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 650
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Book Description
Data on the meteorological parameters pertinent to the aircraft icing problem are so summarized as to give the frequency of occurrence of observed icing situations according to two of the parameters. The summarized data indicate that statistical relations exist between some of the parameters. A method, based upon the collection efficiency of an airfoil and the frequency occurrence of icing situations with various liquid-water contents and mean-effective droplet sizes, is proposed for the selection of design criterions for ice-protection equipment. The method provides a convenient means of calculating the percenteage of icing encounters in which the water collection exceeds the design rate.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1138
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 778
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Book Description
Author: United States. Defense Production Administration
Publisher:
ISBN:
Category : Defense industries
Languages : en
Pages : 752
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Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 996
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Book Description
