NACA-TR-713

Internal-flow systems for aircraft

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:46:59Z
date available	2017-09-04T15:46:59Z
date copyright	01/01/1941
date issued	1941
identifier other	PWWUYDAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/49767
description abstract	An investigation has been made to determine efficient arrangements for an internal-flow system of an aircraft when such a system operates by itself or in combination with other flow systems. The investigation included a theoretical treatment of the problem and tests in the NACA 5-foot vertical wind tunnel of inlet and outlet openings in a flat plate and in a wing.
language	English
title	NACA-TR-713	num
title	Internal-flow systems for aircraft	en
type	standard
page	33
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1941
contenttype	fulltext
subject keywords	AERODYNAMIC
subject keywords	AIR
subject keywords	AIRCRAFT
subject keywords	CONFIGURATIONS
subject keywords	DESIGN
subject keywords	FLOW
subject keywords	INLET
subject keywords	INTAKES
subject keywords	TESTS
subject keywords	TUNNEL
subject keywords	WIND