Abo Bibliothek: Guest

EXPERIMENTAL MODEL STUDIES OF THE EFFECTS OF JET FLOWS ON THE LAUNCH VEHICLE AND LAUNCH PAD WITH A SHORT EXHAUST CHANNEL

Volumen 51, Ausgabe 5, 2020, pp. 545-562
DOI: 10.1615/TsAGISciJ.2021037773
Get accessGet access

ABSTRAKT

This article presents the results of experimental model studies of gas-dynamic, thermal, and acoustic loads on the elements of a launch vehicle and launch pad when using the CX-36 launch complex with a short exhaust channel. The data obtained to date are of significant interest to specialists in the field of space rocket engineering.

REFERENZEN
  1. Antokhin, P.S., Arykhov, Yu.B., Ganabov, V.I., Gusev, V.P., Drozdov, S.M., Zhilin, Yu.V., Zhirnikov, B.L., Ivanov, A.N., Kazanskii, R.A., Krokhin, A.S., Kudin, O.K., Leites, E.A., Loboda, V.L., Marushkin, M.F., Nesterov, Yu.N., Pokhvalinskii, S.M., Stolyarov, E.P., and Shamshurin, A.A., Model Experimental Studies of Gasdynamics, Heat Transfer and Acoustics under Impact of High Temperature Jets of Rocket Engines on a Launch Facility with an Exhaust Channel, Trudy TsAGI, no. 2786, 2019.

  2. Petrov, G.I., Likhushin, V.Ya., Nekrasov, I.P., and Sorkin, L.I., Viscosity Effect on a Supersonic Flow with Shock Waves, Trudy CIAM, no. 224, 1952.

  3. Lipnitskiy, Yu.M. and Safronov, A.V., Ground Testing of the Launch Vehicle Acoustics, TsAGI Sci. J., vol. 45, nos. 3-4, pp. 237-254,2014.

Neueste Ausgabe

KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER Andrei Valerievich Novikov, Alexander Vitalyevich Fedorov, Ivan Vladimirovich Egorov, Anton Olegovich Obraz, Nikolay Nikolaevich Semenov ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION Vladimir Anatolievich Sabelnikov, Vladimir Viktorovich Vlasenko, Sergey Sergeyevich Molev EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE Eduard Borisovich Vasilevskii, Ivan Valeryevich Ezhov, Pavel Vladimirovich Chuvakhov ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE Georgiy Nikolaevich Dudin, Aleksey Vyacheslavovich Ledovskiy WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT Vladimir Alekseevich Zharov, Igor Ivanovich Lipatov, Rami Salah Saber Selim NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION Viktor Viktorovich Vyshinsky, Koang T'in' Zoan POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS Timur Romanovich Zuev, Mikhail Semenovich Tararyshkin A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR Maxim Andreyevich Ledyankin , Sergey Anatolyevich Mikhailov, Dmitry Valeryevich Nedel'ko, Timur Arturovich Agliullin INDEX, VOLUME 51, 2020
Digitales Portal Digitale Bibliothek eBooks Zeitschriften Referenzen und Berichte Forschungssammlungen Preise und Aborichtlinien Begell House Kontakt Language English 中文 Русский Português German French Spain