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NASA-TN-D-7205

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:13:08Z
date available2017-09-04T17:13:08Z
date copyright01/01/1973
date issued1973
identifier otherYXITDEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/136634
description abstractAn investigation has been conducted to determine the effects of flap span and wing aspect ratio on the static longitudinal aerodynamic characteristics and chordwise and spanwise pressure distributions on the wing and trailing-edge flap of a straight-wing STOL model having an externally blown jet flap without vertical and horizontal tail surfaces. The force tests were made over an angle-of-attack range for several thrust coefficients and two flap deflections. The pressure data are presented as tabulated and plotted chordwise pressure-distribution coefficients for angles of attack of 1 and 16. Pressure-distribution measurements were made at several spanwise stations.
languageEnglish
titleNASA-TN-D-7205num
titleEffect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL modelen
typestandard
page139
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1973
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAIRCRAFT
subject keywordsBLOWN
subject keywordsCHARACTERISTICS
subject keywordsCOEFFICIENTS
subject keywordsCONFIGURATIONS
subject keywordsDISTRIBUTION
subject keywordsEXTERNALLY
subject keywordsFLAPS
subject keywordsFLOW
subject keywordsMODELS
subject keywordsPRESSURE
subject keywordsSHORT
subject keywordsSTATIC
subject keywordsTAKEOFF
subject keywordsTUNNEL
subject keywordsWIND


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