Inscrição na biblioteca: Guest
Portal Digital Begell Biblioteca digital da Begell eBooks Diários Referências e Anais Coleções de pesquisa
TsAGI Science Journal

ISSN Imprimir: 1948-2590
ISSN On-line: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2013007838
pages 111-127

NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF THE HYPERSONIC AIRCRAFT MODEL OF INTEGRATED CONFIGURATION

Sergey Mikhailovich Zadonsky
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia
Alexander Petrovich Kosykh
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia
Garry Grantovich Nersesov
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia
Iraida Fedorovna Chelysheva
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia
Sergey Valer'evich Chernov
Central Aerohydrodynamic Institute (TsAGI), Zhukovsky str. 1, Zhukovsky, Moscow Region, 140180 Russia
Vladimir L'vovich Yumashev
Central Aerohydrodynamic Institute (TsAGI) 1, Zhukovsky str., Zhukovsky, 140180, Moscow region, Russia

RESUMO

Numerical simulation of inviscid flow over three hypersonic aircrafts of different idealized configurations with flow through the contoured duct of the air-jet engine has been performed at M∞ = 6 and α = 0−10°. The Influence of the front jaws of the air intake on the aerodynamic characteristics of the aircraft with a blunt wedged fuselage has been considered. The effect of different elements of the hypersonic aircraft on the aerodynamic characteristics has been estimated. Numerical data have been supplemented with the results of the experiments carried out in the wind tunnel at TsAGI.


Articles with similar content:

INVESTIGATIONS OF FLOW PARAMETERS IN MODELS OF PRECOMBUSTION DIFFUSERS WITH SECTIONED DUCTS
TsAGI Science Journal, Vol.50, 2019, issue 1
Mikhail Anatolyevich Ivankin, Natalya Valeryevna Guryleva, Aleksander Mikhailovich Tereshin, Dmitry Aleksandrovich Lapinsky
COMPUTATIONAL INVESTIGATION OF BLADE SAILING PHENOMENON BY FLUID STRUCTURE INTERACTION APPROACH
Proceedings of the 24th National and 2nd International ISHMT-ASTFE Heat and Mass Transfer Conference (IHMTC-2017), Vol.0, 2017, issue
Asif Ali, Shrish Shukla, Sidh Nath Singh
INVESTIGATION OF LAMINAR–TURBULENT TRANSITION ON THE WING SECTION AT VARIOUS REYNOLDS NUMBERS
TsAGI Science Journal, Vol.48, 2017, issue 2
Andrey Filippovich Kiselev, Valery Viktorovich Vozhdaev, Leonid Leonidovich Teperin, Petr Petrovich Vorotnikov, Leonid Leonidovich Chernyshev
ESTIMATION OF OPERATING CONDITIONS OF A MID-RANGE AIRCRAFT AUXILIARY POWER UNIT WITH RECEIVER INLET IN TURBULENT FLOW
TsAGI Science Journal, Vol.46, 2015, issue 4
Egor Vyacheslavovich Kazhan, Vladimir Fedorovich Tretyakov, Evgenii Petrovich Bykov
BUFFET INTENSITY REDUCTION OF A COMBAT AIRCRAFT WING
TsAGI Science Journal, Vol.47, 2016, issue 2
Robert Galimovich Abdrashitov, Igor Borisovich Chuchkalov, Vladimir Anatolyevich Pesetsky