contributor author | J. M. Seiner | |
contributor author | J. C. Manning | |
contributor author | F. J. Capone | |
contributor author | O. C. Pendergraft | |
date accessioned | 2017-05-08T23:38:19Z | |
date available | 2017-05-08T23:38:19Z | |
date copyright | October, 1992 | |
date issued | 1992 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26709#816_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/110191 | |
description abstract | The origin of dynamic pressure loads on external divergent engine nozzle flaps of the B-1B aircraft was investigated in the NASA/LaRC 16-ft transonic tunnel using a 6 percent full-span model with powered engine nacelles. External flap dynamic loads and afterbody drag associated with flap removal were measured using this model. Both dry and maximum A/B power nozzles were evaluated in this study. As a result of this study, the principle mechanisms responsible for high dynamic external flap loads were determined along with performance penalty associated with flap removal. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Study of External Dynamic Flap Loads on a 6 Percent B-1B Model | |
type | Journal Paper | |
journal volume | 114 | |
journal issue | 4 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.2906662 | |
journal fristpage | 816 | |
journal lastpage | 828 | |
identifier eissn | 0742-4795 | |
keywords | Stress | |
keywords | Nozzles | |
keywords | Engines | |
keywords | Drag (Fluid dynamics) | |
keywords | Pressure | |
keywords | Aircraft | |
keywords | Tunnels AND Mechanisms | |
tree | Journal of Engineering for Gas Turbines and Power:;1992:;volume( 114 ):;issue: 004 | |
contenttype | Fulltext | |