Show simple item record

NACA-RM-E53E28

Experimental investigation of the effects of support interference on the pressure distribution of a body of revolution at a Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 14 x 10(exp 6)

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:51:57Z
date available2017-09-04T15:51:57Z
date copyright01/01/1953
date issued1953
identifier otherQLMCWDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/55184
description abstractA compilation of available information on the problem of support interference at transonic and supersonic speeds is presented. (author)
languageEnglish
titleNACA-RM-E53E28num
titleExperimental investigation of the effects of support interference on the pressure distribution of a body of revolution at a Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 14 x 10(exp 6)en
typestandard
page19
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1953
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsAFTERBODIES
subject keywordsANGLE
subject keywordsATTACK
subject keywordsBASE
subject keywordsBODIES
subject keywordsCONICAL
subject keywordsCYLINDRICAL
subject keywordsFINNED
subject keywordsFOREBODIES
subject keywordsGEOMETRY
subject keywordsINTERFERENCE
subject keywordsMODELS
subject keywordsPRESSURE
subject keywordsPROTUBERANCES
subject keywordsREVOLUTION
subject keywordsSPEED
subject keywordsSUPERSONIC
subject keywordsSUPPORTS
subject keywordsSURFACE
subject keywordsTESTS
subject keywordsTRANSONIC
subject keywordsTUNNEL
subject keywordsTUNNELS
subject keywordsWIND


Files in this item

Thumbnail
Name:
QLMCWDAAAAAAAAAA.pdf
Size:
362.3Kb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record