NASA-MEMO-12-1-58 REV A

Estimation of Directional Stability Derivatives at Moderate Angles and Supersonic Speeds

contributor author	NASA - National Aeronautics and Space Administration (NASA)
date accessioned	2017-09-04T16:15:57Z
date available	2017-09-04T16:15:57Z
date copyright	01/01/1959
date issued	1959
identifier other	SYMKAEAAAAAAAAAA.pdf
identifier uri	https://yse.yabesh.ir/std/handle/yse/79255
description abstract	A study of some of the important aerodynamic factors affecting the directional stability of supersonic airplanes is presented. The mutual interference fields between the body, the lifting surfaces, and the stabilizing surfaces are analyzed in detail. Evaluation of these interference fields on an approximate theoretical basis leads to a method for predicting directional stability of supersonic airplanes. Body shape, wing position and plan form, vertical tail position and plan form, and ventral fins are taken into account. Estimates of the effects of these factors are in fair agreement with experiment.
language	English
title	NASA-MEMO-12-1-58 REV A	num
title	Estimation of Directional Stability Derivatives at Moderate Angles and Supersonic Speeds	en
type	standard
page	74
status	Active
tree	NASA - National Aeronautics and Space Administration (NASA):;1959
contenttype	fulltext