NASA-CR-165768

Design and analysis of a fuel-efficient single-engine, turboprop-powered, business airplane

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T15:35:40Z
date available	2017-09-04T15:35:40Z
date copyright	01/01/1981
date issued	1981
identifier other	AYMKAEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/37580
description abstract	The speed, range, payload, and fuel efficiency of a general aviation airplane powered by one turboprop engine was determined and compared to a twin engine turboprop aircraft. An airplane configuration was developed which can carry six people for a noreserve range of 2,408 km at a cruise speed above 154 m/s, and a cruise altitude of about 9,144 m. The cruise speed is comparable to that of the fastest of the current twin turboprop powered airplanes. It is found that the airplane has a cruise specific range greater than all twin turboprop engine airplanes flying in its speed range and most twin piston engine airplanes flying at considerably slower cruise airspeeds.
language	English
title	NASA-CR-165768	num
title	Design and analysis of a fuel-efficient single-engine, turboprop-powered, business airplane	en
type	standard
page	42
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1981
contenttype	fulltext