The Cumulative Exceedance Distribution for Accelerations Due to Turbulence Encountered by a CT/4A Air Trainer

A gust load spectrum is estimated for a CT/4A Airtrainer. The spectrum will be used in the specification of a loading sequence for a fatigue test. The accuracy of the estimation method is tested by comparing observed and predicted gust load spectra for the Aero-commander 680. (Author)

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Main Author: Sherman,D J
Format: Report
Language:English
Subjects:
Acceleration
Aerocommander-680 aircraft
Aerodynamic loading
Aerodynamics
Australia
Estimates
Experimental data
Fatigue tests(Mechanics)
Gust loads
Mathematical prediction
Profiles
Spectra
Subsonic flight
Training Aircraft
Turbulence
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description A gust load spectrum is estimated for a CT/4A Airtrainer. The spectrum will be used in the specification of a loading sequence for a fatigue test. The accuracy of the estimation method is tested by comparing observed and predicted gust load spectra for the Aero-commander 680. (Author)
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(Author)</description><subject>Acceleration</subject><subject>Aerocommander-680 aircraft</subject><subject>Aerodynamic loading</subject><subject>Aerodynamics</subject><subject>Australia</subject><subject>Estimates</subject><subject>Experimental data</subject><subject>Fatigue tests(Mechanics)</subject><subject>Gust loads</subject><subject>Mathematical prediction</subject><subject>Profiles</subject><subject>Spectra</subject><subject>Subsonic flight</subject><subject>Training Aircraft</subject><subject>Turbulence</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1983</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNqFi0EKwjAQRbtxIeoNXMwFRKXVfUgrHiD7kqZTHEgTmMyI3l4L7l19eO_9dTW7B4LVWaMXeiJ0r4A4-hQQWirCNKhQTjBlBhMCRmS_gAKtIkgGpzxoxOXQpZA1CTKOMLzBg3XHxoAhBseeEvK2Wk0-Ftz9dlPtb52z98MoFPoi30Z605pzfbk2p_qP_gBSxT3d</recordid><startdate>198308</startdate><enddate>198308</enddate><creator>Sherman,D J</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>198308</creationdate><title>The Cumulative Exceedance Distribution for Accelerations Due to Turbulence Encountered by a CT/4A Air Trainer</title><author>Sherman,D J</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_ADA1356403</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1983</creationdate><topic>Acceleration</topic><topic>Aerocommander-680 aircraft</topic><topic>Aerodynamic loading</topic><topic>Aerodynamics</topic><topic>Australia</topic><topic>Estimates</topic><topic>Experimental data</topic><topic>Fatigue tests(Mechanics)</topic><topic>Gust loads</topic><topic>Mathematical prediction</topic><topic>Profiles</topic><topic>Spectra</topic><topic>Subsonic flight</topic><topic>Training Aircraft</topic><topic>Turbulence</topic><toplevel>online_resources</toplevel><creatorcontrib>Sherman,D J</creatorcontrib><creatorcontrib>AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Sherman,D J</au><aucorp>AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>The Cumulative Exceedance Distribution for Accelerations Due to Turbulence Encountered by a CT/4A Air Trainer</btitle><date>1983-08</date><risdate>1983</risdate><abstract>A gust load spectrum is estimated for a CT/4A Airtrainer. 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source DTIC Technical Reports
subjects Acceleration
Aerocommander-680 aircraft
Aerodynamic loading
Aerodynamics
Australia
Estimates
Experimental data
Fatigue tests(Mechanics)
Gust loads
Mathematical prediction
Profiles
Spectra
Subsonic flight
Training Aircraft
Turbulence
title The Cumulative Exceedance Distribution for Accelerations Due to Turbulence Encountered by a CT/4A Air Trainer
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