NASA-TN D-6800

Longitudinal aerodynamic characteristics of light, twin-engine, propeller-driven airplanes

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:59:26Z
date available	2017-09-04T16:59:26Z
date copyright	06/01/1972
date issued	1972
identifier other	XLYKAEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/122894
description abstract	Representative state-of-the-art analytical procedures and design data for predicting the longitudinal static and dynamic stability and control characteristics of light, propeller-driven airplanes are presented. Procedures for predicting drag characteristics are also included. The procedures are applied to a twin-engine, propeller-driven airplane in the clean configuration from zero lift to stall conditions. The calculated characteristics are compared with wind-tunnel and flight data. Included in the comparisons are level-flight trim characteristics, period and damping of the short-period oscillatory mode, and windup-turn characteristics. All calculations are documented.
language	English
title	NASA-TN D-6800	num
title	Longitudinal aerodynamic characteristics of light, twin-engine, propeller-driven airplanes	en
type	standard
page	374
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1972
contenttype	fulltext