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Ground distance covered during airborne horizontal deceleration of an airplane

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:39:48Z
date available2017-09-04T16:39:48Z
date copyright01/01/1978
date issued1978
identifier otherVMBBFEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/103486
description abstractThe distance an airplane floats with respect to the ground during deceleration at constant altitude is analyzed taking into account the effects of a constant wind. By use of suitable nondimensionalizing parameters, data applicable to all airplanes are presented by means of a single family of curves.
languageEnglish
titleNASA-TP-1157num
titleGround distance covered during airborne horizontal deceleration of an airplaneen
typestandard
page14
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1978
contenttypefulltext
subject keywordsAIRCRAFT LANDING
subject keywordsDECELERATION
subject keywordsDRAG REDUCTION
subject keywordsFLOATING
subject keywordsGENERAL AVIATION AIRCRAFT
subject keywordsGROUND EFFECT (AERODYNAMICS)
subject keywordsGROUND WIND
subject keywordsLANDING LOADS
subject keywordsLANDING SPEED
subject keywordsLIFT


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