NACA-TN-3668

Preliminary investigation of a family of diffusers designed for near sonic inlet velocities

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:15:17Z
date available	2017-09-04T16:15:17Z
date copyright	01/01/1956
date issued	1956
identifier other	SWNUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/78505
description abstract	Tests have been conducted with a series of diffuser shapes defined by empirical equations having constants which are related to the initial boundary-layer thickness. The shapes were designed to provide high pressure recovery at near sonic inlet Mach numbers, and tests were conducted through the mass-flow range with a variety of attached and separated initial boundary layers. Tests were also conducted with two offset ducts and with a variety of surface conditions in the shortest duct.
language	English
title	NACA-TN-3668	num
title	Preliminary investigation of a family of diffusers designed for near sonic inlet velocities	en
type	standard
page	44
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1956
contenttype	fulltext