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NACA-TR-1307

Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:58:53Z
date available2017-09-04T17:58:53Z
date copyright01/01/1957
date issued1957
identifier otherFSUYYDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/182056
description abstractA method is presented for calculating the lift and centers of pressure of wing-body and wing-body-tail combinations at subsonic, transonic, and supersonic speeds. A set of design charts and a computing table are presented which reduce the computations to routine operations. Comparison between the estimated and experimental characteristics for a number of wing-body and wing-body-tail combinations shows correlation to within or - 10 percent on lift and to within about or - 0.02 of the body length on center of pressure.
languageEnglish
titleNACA-TR-1307num
titleLift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speedsen
typestandard
page70
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1957
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAERODYNAMICS
subject keywordsAIRCRAFT
subject keywordsBODIES
subject keywordsBODY
subject keywordsCENTER
subject keywordsCIRCULAR
subject keywordsCOMPONENTS
subject keywordsCOMPUTATIONAL
subject keywordsCONFIGURATIONS
subject keywordsCYLINDERS
subject keywordsCYLINDRICAL
subject keywordsDYNAMICS
subject keywordsFLUID
subject keywordsINTERACTIONAL
subject keywordsINTERFERENCE
subject keywordsLIFT
subject keywordsMISSILE
subject keywordsPRESSURE
subject keywordsRECTANGULAR
subject keywordsSPEED
subject keywordsSUBSONIC
subject keywordsSUPERSONIC
subject keywordsSURFACES
subject keywordsTAIL
subject keywordsTRANSONIC
subject keywordsTRAPEZOIDAL
subject keywordsWING
subject keywordsWINGS


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