NACA-TN-3583

Charts of boundary-layer mass flow and momentum for inlet performance analysis mach number range, 0.2 to 5.0

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:10:08Z
date available	2017-09-04T18:10:08Z
date copyright	01/01/1955
date issued	1955
identifier other	GWNUYDAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/193172
description abstract	Mass flow and momentum for various fractions of a turbulent boundary layer are presented in chart form for a range of velocity profiles and for Mach numbers from 0.2 to 5.0. These charts are intended to assist the analyst and designer of boundary,layer removal systems. Application of the charts to inlets of arbitrary shape and to the determination of the pressure recovery of rectangular, normal-shock inlets immersed in boundary layer is described.
language	English
title	NACA-TN-3583	num
title	Charts of boundary-layer mass flow and momentum for inlet performance analysis mach number range, 0.2 to 5.0	en
type	standard
page	27
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1955
contenttype	fulltext