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Exploratory investigation at Mach number 4.06 of an airplane configuration having a wing of trapezoidal plan form effects of various tail arrangements on wing-on and wing-off static longitudinal and lateral stability characteristics

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:18:06Z
date available2017-09-04T18:18:06Z
date copyright01/01/1955
date issued1955
identifier otherHQSWXDAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/200865
description abstractINTRODUCTION
The airplane configurations previously investigated experimentally at high supersonic and hypersonic speeds have been restricted to misssile types which were not required to land and which, therefore, had relatively small wings or wings of very low aspect ratio. The purpose of the present investigation is to determine the characteristics of a configuration conforming more closely to a piloted airplane having a wing area sufficient for conventional landing.
In references 2, 3, and 4 longitudinal and lateral stability data were presented, and in references 5 and 6 longitudinal and lateral control data were presented for this airplane configuration and various combinations of its components at Mach numbers of 4 .06 and 6.86. This report presents, at a Mach number of 4.06, the effects of various combinations of the horizontal and vertical tails on the airplane with and without the wing. The data have been analyzed only to the extent that some stability determinants have been obtained.
languageEnglish
titleNACA-RM-L55D08num
titleExploratory investigation at Mach number 4.06 of an airplane configuration having a wing of trapezoidal plan form effects of various tail arrangements on wing-on and wing-off static longitudinal and lateral stability characteristicsen
typestandard
page61
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1955
contenttypefulltext


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