NASA-RP-1060

Subsonic aircraft: Evolution and the matching of size to performance

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T18:32:34Z
date available	2017-09-04T18:32:34Z
date copyright	01/01/1980
date issued	1980
identifier other	JBNKAEAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho146/handle/yse/214702
description abstract	Methods for estimating the approximate size, weight, and power of aircraft intended to meet specified performance requirements are presented for both jet-powered and propeller-driven aircraft. The methods are simple and require only the use of a pocket computer for rapid application to specific sizing problems. Application of the methods is illustrated by means of sizing studies of a series of jet-powered and propeller-driven aircraft with varying design constraints. Some aspects of the technical evolution of the airplane from 1918 to the present are also briefly discussed.
language	English
title	NASA-RP-1060	num
title	Subsonic aircraft: Evolution and the matching of size to performance	en
type	standard
page	447
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1980
contenttype	fulltext