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NACA-TR-1051

An analysis of base pressure at supersonic velocities and comparison with experiment

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1951

Abstract: In the first part of the investigation an analysis is made of base pressure in an inviscid fluid, both for two-dimensional and axially symmetric flow. It is shown that for two-dimensional flow, and also for the flow over a body of revolution with a cylindrical sting attached to the base, there are an infinite number of possible solutions satisfying all necessary boundary conditions at any given free-stream Mach number. For the particular case of a body having no sting attached only one solution is possible in an inviscid flow, but it corresponds to zero base drag. Accordingly, it is concluded that a strictly inviscid-fluid theory cannot be satisfactory for practical applications. An approximate semi-empirical analysis for base pressure in a viscous fluid is developed in a second part of the investigation. The semi-empirical analysis is based partly on inviscid-flow calculations.
URI: https://yse.yabesh.ir/std/handle/yse/30518
Subject: AERODYNAMIC
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    NACA-TR-1051

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:29:19Z
date available2017-09-04T15:29:19Z
date copyright01/01/1951
date issued1951
identifier otherNXDZYDAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/30518
description abstractIn the first part of the investigation an analysis is made of base pressure in an inviscid fluid, both for two-dimensional and axially symmetric flow. It is shown that for two-dimensional flow, and also for the flow over a body of revolution with a cylindrical sting attached to the base, there are an infinite number of possible solutions satisfying all necessary boundary conditions at any given free-stream Mach number. For the particular case of a body having no sting attached only one solution is possible in an inviscid flow, but it corresponds to zero base drag. Accordingly, it is concluded that a strictly inviscid-fluid theory cannot be satisfactory for practical applications. An approximate semi-empirical analysis for base pressure in a viscous fluid is developed in a second part of the investigation. The semi-empirical analysis is based partly on inviscid-flow calculations.
languageEnglish
titleNACA-TR-1051num
titleAn analysis of base pressure at supersonic velocities and comparison with experimenten
typestandard
page25
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1951
contenttypefulltext
subject keywordsAERODYNAMIC
subject keywordsANALYSIS
subject keywordsAXISYMMETRIC
subject keywordsBASE
subject keywordsBODIES
subject keywordsBOUNDARY
subject keywordsBOW
subject keywordsCOMPARISON
subject keywordsCYLINDRICAL
subject keywordsDRAG
subject keywordsFLOW
subject keywordsFREE
subject keywordsINTERFERENCE
subject keywordsINVISCID
subject keywordsLAMINAR
subject keywordsLAYER
subject keywordsMACH
subject keywordsMATHEMATICS
subject keywordsNUMBER
subject keywordsPRESSURE
subject keywordsPROBLEMS
subject keywordsPROFILES
subject keywordsREVOLUTION
subject keywordsREYNOLDS
subject keywordsSHAPES
subject keywordsSUPERSONIC
subject keywordsSUPPORTS
subject keywordsTESTS
subject keywordsTRANSITION
subject keywordsTUNNEL
subject keywordsTUNNELS
subject keywordsTURBULENT
subject keywordsVALUE
subject keywordsVISCOUS
subject keywordsWAVES
subject keywordsWIND
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