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NACA-TN-1743

Flight measurements of the stability, control, and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-span slots and a comparison with wind-tunnel data

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:58:46Z
date available2017-09-04T15:58:46Z
date copyright01/01/1948
date issued1948
identifier otherRDPTYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/61907
description abstractFlight measurements have been made to determine the low-speed flying qualities of an airplane having a wing swept back 35° at the quarter-chord line. The lateral and detections stability and control characteristics of the airplane without slots and with 80-percent-span slots on the wing are presented. Also included are measurements of the longitudinal stability, stalling, and lift characteristics with 80- percent span slots. Tests were made both with and without a ventral-fin extension on the airplane.
languageEnglish
titleNACA-TN-1743num
titleFlight measurements of the stability, control, and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-span slots and a comparison with wind-tunnel dataen
typestandard
page86
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1948
contenttypefulltext
subject keywordsAIRPLANES
subject keywordsCHARACTERISTICS
subject keywordsCONTROL
subject keywordsDIHEDRAL
subject keywordsDIRECTIONAL
subject keywordsFLYING
subject keywordsLATERAL
subject keywordsLONGITUDINAL
subject keywordsQUALITIES
subject keywordsSIDESLIPPING
subject keywordsSLOTS
subject keywordsSTABILITY
subject keywordsSTALLING
subject keywordsSTATIC
subject keywordsSWEPTBACK
subject keywordsWING
subject keywordsWINGS


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