NASA-TN-D-71

An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:44:58Z
date available	2017-09-04T15:44:58Z
date copyright	01/01/1959
date issued	1959
identifier other	PQTKAEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/47434
description abstract	The effects of profile curvature on the flow over blunt plates was investigated. A method of calculating surface pressures was developed which utilized a combination of viscous andinviscid hypersonic parameters. The method was assessed by comparison to experiment conducted in air and helium over a range of Mach numbers from 4 to 13.3 and leading-edge Reynolds numbers from 6,600 to 129,000 for elliptic and circular leading edges.
language	English
title	NASA-TN-D-71	num
title	An approximate method for calculating surface pressures on curved profile blunt plates in hypersonic flow	en
type	standard
page	28
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1959
contenttype	fulltext