NACA-TM-1382

Steady properly-banked turns of turbojet-propelled airplanes

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:52:33Z
date available	2017-09-04T16:52:33Z
date copyright	01/01/1955
date issued	1955
identifier other	WTONEEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/116121
description abstract	The problem of a jet-propelled airplane held in a steady turn is treated both in the very general case and also in the particular case when the polar curve can be approximated by a parabola. Once the general solution has been obtained, some typical maneuvers are next studied such as, the turn of maximum bank, of maximum angular velocity, and of minimum radius of curvature. After a brief comparison is made between the turning characteristics of conventional airplanes and jet airplanes, and after the effect of compressibility upon the turn is examined, the effects of the salient aerodynamic and structural parameters upon the behavior of the plane in curvilinear flight are summarized in the conclusions.
language	English
title	NACA-TM-1382	num
title	Steady properly-banked turns of turbojet-propelled airplanes	en
type	standard
page	34
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1955
contenttype	fulltext