PROCESS OF PRODUCTION OF HYPERSONIC FLOW Russian patent published in 1998 - IPC

Abstract RU 2101691 C1

FIELD: production of high-energy flows of working gas suitable for modeling of hypersonic flight in atmosphere of the Earth under ground conditions. SUBSTANCE: process of production of hypersonic flow consists in preliminary acceleration of gas in expanding part of Laval nozzle to Mach number 4-6 and its subsequent acceleration in cylindrical part of nozzle by removal of heat from flow. Thanks to this there is provided creation of high-speed flow of gas with high actual values of modeling parameters, namely, with high pressure of deceleration of flow under normal value of gas pressure in prechamber. EFFECT: simplified design of installation for production of hypersonic gas flows, saving of energy resources. 1 dwg

Similar patents RU2101691C1

Title Year Author Number
AERODYNAMIC TUNNEL 2000
  • Topchijan M.E.
  • Pinakov V.I.
  • Meshcherjakov A.A.
  • Kurshin A.P.
RU2166186C1
METHOD OF DETERMINATION OF THE CONTROL SIGNAL ON THE CORNER OF THE ROLL MODEL OF THE HYPERPOWER VEHICLE EQUIPMENT (HVE) FOR MONITORING THE AERODYNAMIC IDENTITY ON THE REINOLDS NUMBER OF TRAJECTORIES OF THE FLIGHT OF THE MODEL AND THE NUCLEAR ARTICLE WHEN CONDUCTING ANTI-STATE AIRCRAFT RESEARCH 2016
  • Lovitskij Lavrentij Lavrentevich
  • Sadrtdinov Vladislav Diyasovich
RU2615220C1
METHOD FOR HYPERSONIC AIRCRAFT (HAC) MODEL ROLL ANGLE GENERATION OF A CONTROL SIGNAL FOR CONTROLLING THE AERODYNAMIC IDENTITY ACCORDING TO THE REYNOLDS NUMBERS OF THE FLIGHT TRAJECTORIES OF THE MODEL AND THE FULL-SCALE AIRCRAFT IN CONDUCTING ADVANCED FLIGHT TESTS OF AERODYNAMIC CHARACTERISTICS 2017
  • Lovitskij Lavrentij Lavrentevich
  • Sadrtdinov Vladislav Diyasovich
  • Badretdinova Ajgul Bulatovna
RU2650331C1
HYPERSONIC SHOCK AERODYNAMIC PIPE 2016
  • Ruleva Larisa Borisovna
  • Kotov Mikhail Altaevich
  • Solodovnikov Sergej Ivanovich
  • Samokhvalov Gennadij Vasilevich
RU2621367C1
METHOD FOR ARRANGEMENT OF WORKING PROCESS IN STRAIGHT-FLOW AIR-JET ENGINE WITH CONTINUOUS-DETONATION COMBUSTION CHAMBER AND DEVICE FOR IMPLEMENTATION THEREOF 2019
  • Frolov Sergej Mikhajlovich
  • Ivanov Vladislav Sergeevich
  • Nabatnikov Sergej Aleksandrovich
  • Zangiev Alan Elbrusovich
  • Avdeev Konstantin Alekseevich
  • Zvegintsev Valerij Ivanovich
  • Shulakova Nadezhda Sergeevna
RU2714582C1
METHOD OF OBTAINING AIR FLOW AT FULL-SCALE PARAMETERS AND DEVICE FOR REALIZATION OF THIS METHOD 1995
  • Vologodskij Vadim Borisovich
RU2093716C1
HEAT EXCHANGER HEATING METHOD OF THE HOUSES HEATING SYSTEM AND OTHER OBJECTS AND DEVICE FOR THE METHOD IMPLEMENTATION 2012
  • Shesterenko Sergej Nikolaevich
RU2618183C2
METHOD FOR PRODUCING IMPACT-COMPRESSED PLASMA LAYER AND DEVICE FOR ITS IMPLEMENTATION 2014
  • Kalashnikov Evgenij Valentinovich
RU2590893C1
METHOD OF GAS FLOW CREATION IN AERODYNAMIC TUNNEL AND AERODYNAMIC TUNNEL 2013
  • Kekhvajants Valerij Grigor'Evich
  • Podlubnyj Viktor Vladimirovich
  • Batura Nikolaj Ivanovich
  • Chistov Julij Ivanovich
RU2526505C1
METHOD TO VARY HYPERSONIC AIRCRAFT AERODYNAMIC CHARACTERISTICS AND DEVICE TO THIS END 2008
  • Nizovtsev Vladimir Mikhajlovich
RU2383469C1

RU 2 101 691 C1

Authors

Zvegintsev Valerij Ivanovich

Dates

1998-01-10Published

1996-01-31Filed