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NACA-RM-L54C16

Experimental effects of propulsive jets and afterbody configurations on the zero-lift drag of bodies of revolution at a Mach number of 1.59

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:07:44Z
date available2017-09-04T18:07:44Z
date copyright01/01/1954
date issued1954
identifier otherGPSWXDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/190670
description abstractThe present investigation was made at a free-stream Mach number of 1.59 to compare the afterbody drags to a series of conical boattailed models at zero angle of attack. Afterbody drags were obtained for both the power-off and the power-on conditions. Power-on drags were obtained as a function of afterbody fineness ratio, jet pressure ratio and divergence, and jet Mach number.
languageEnglish
titleNACA-RM-L54C16num
titleExperimental effects of propulsive jets and afterbody configurations on the zero-lift drag of bodies of revolution at a Mach number of 1.59en
typestandard
page34
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1954
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANGLE
subject keywordsANGLES
subject keywordsATTACK
subject keywordsBASE
subject keywordsBOATTAILS
subject keywordsBODIES
subject keywordsCONICAL
subject keywordsDISTRIBUTION
subject keywordsDRAG
subject keywordsEXHAUST
subject keywordsFLOW
subject keywordsFREE
subject keywordsGEOMETRY
subject keywordsINTERFERENCE
subject keywordsJET
subject keywordsLIFT
subject keywordsMACH
subject keywordsNOZZLES
subject keywordsNUMBER
subject keywordsPRESSURE
subject keywordsRATIO
subject keywordsREVOLUTION
subject keywordsZERO


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