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NASA-TN-D-30

Flight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type Airplane

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1960

Abstract: The lift and drag characteristics of a Boeing KC-135 airplane were determined during maneuvering flight over the Mach number range from 0.70 to 0.85 for the airplane in the clean configuration at an altitude of 26,000 feet. Data were also obtained over the speed range of 130 knots to 160 knots at 9,000 feet for various flap deflections with gear down.
URI: https://yse.yabesh.ir/std/handle/yse/21466
Subject: AERODYNAMIC CHARACTERISTICS
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    NASA-TN-D-30

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:21:30Z
date available2017-09-04T15:21:30Z
date copyright01/01/1960
date issued1960
identifier otherMZHOEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/21466
description abstractThe lift and drag characteristics of a Boeing KC-135 airplane were determined during maneuvering flight over the Mach number range from 0.70 to 0.85 for the airplane in the clean configuration at an altitude of 26,000 feet. Data were also obtained over the speed range of 130 knots to 160 knots at 9,000 feet for various flap deflections with gear down.
languageEnglish
titleNASA-TN-D-30num
titleFlight Investigation of the Lift and Drag Characteristics of a Swept-Wing, Multijet, Transport-Type Airplaneen
typestandard
page30
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1960
contenttypefulltext
subject keywordsAERODYNAMIC CHARACTERISTICS
subject keywordsAERODYNAMIC COEFFICIENTS
subject keywordsAERODYNAMIC CONFIGURATIONS
subject keywordsAERODYNAMIC DRAG
subject keywordsC-135 AIRCRAFT
subject keywordsFLIGHT TESTS
subject keywordsJET AIRCRAFT
subject keywordsLIFT
subject keywordsMACH NUMBER
subject keywordsMANEUVERS
subject keywordsSUBSONIC SPEED
subject keywordsSWEPT WINGS
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DSpace software copyright © 2017-2020  DuraSpace
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