Article
Cover
Title
Investigation of force and thermal loading of jet deflectors of launch complexes of space rockets during the work of water supply systemsAuthors
B.E. Sinilshchikov, V.B. SinilshchikovOrganization
Baltic State Technical University «VOENMEH» named after D .F. UstinovSaint Petersburg, Russian Federation
Abstract
In the most of modern launch complexes of space rockets the water supply systems are used to defend the surfaces acted directly upon by high-temperature jet flows from melting. The paper presents the estimation for parameters of force and heat loads of jet deflector during the work of intra-jet and extrajet water supply systems. The method of numerical simulation for two-phase gas-droplet flows is used. The description of a mathematical model is given. For description of gas flow the Navier-Stokes equations completed with an algebraic model of turbulence are applied, this model being similar to the Prandtl one but taking into account the influence of a droplet phase. Thermodynamic parameters are determined by the model of ideal gas for a mechanical mixture of three components: combustion products, atmospheric air, and vapor (steam) formed as a result of water evaporation. The flow of a droplet phase is calculated on the base of continual approach with using the elements of trajectory approach. The resistance, evaporation of droplets, and droplet breakup are taken into consideration. The calculation is performed for the range from the nozzle section of the rocket engine to the jet deflector. The values of heat flows in the surface are estimated by means of the parameters of a gas-droplet flow impinging upon a barrier. The results of calculation are presented for the versions which differ in the scheme of water supply systems, disposition of branch tubes, and spray velocity and dispersability.Keywords
rocket engine, jet, jet deflector, water supply, heat flows, evaporation, breakupReferences
[1] Tekhnologicheskiye ob’ekty nazemnoy infrastruktury raketno-kosmicheskoy tekhniki [Technological objects of ground-based infrastructure of rocket-and-space engineering]. Engineering manual. Book 1. Edited by I. V. Barmin. Moscow, Poligraphiks-RPK Publ., 2005, 416 p. (In Russian)
[2] Biryukov G. P., But A. B., Khotulev V. A., Fadeev A. S. Gazodinamika startovykh kompleksov [Gasdynamics starting complexes]. Moscow, Restart Publ., 2012, 364 p. (In Russian)
[3] Degtyar’ V. G., Merkulov E. S., Safronov A. V., Khlybov V. I. Rezul’taty raschetno-eksperimentalnykh issledovaniy gazodinamicheskikh protsessov pri vzaimodeistvii mnogoblochnykh struy raketnykh dvigateley s gazootrazhatelem startovogo sooruzheniya [Results of calculation and experimental studies of gas-dynamic processes in the interaction of multi-block jets of rocket engines with the gas reflector of the launch facility]. Kosmonavtika i raketostroeniye, № 1 (70), 2013, pp. 37–45. (In Russian)
[4] Safronov A. V., Kravchuk M. O., Abdurashidov T. O., But A. B. Raschetnye issledovaniya gazodinamiki starta v obespecheniye sozdaniya SK RN sverkhtyazhelogo klassa [Calculation studies of the gasdynamics of the launch in ensuring the creation of the launch complex of the super-heavy-class launch vehicle]. Sbornik trudov XLI Akademicheskikh chteniy po kosmonavtike. Moscow, MGTU im Baumana Publ., 2017. (In Russian)
[5] Jeff West, Louise L. Strutzenberg, Gabriel C. Putnam, Peter A. Liever, Brandon R. Williams. Development of Modeling Capabilities for Launch Pad Acoustics and Ignition Transient Environment Prediction. 18th AIAA/CEAS Aeroacoustics Conference; Colorado Springs, CO; 4-6 Jun. 2012; United States 33rd AIAA Aeroacoustics Conference; Colorado Springs, CO; 4–6 Jun. 2012.
[6] Volkov K. N., Emel’yanov V. N. Techeniya gaza s chastitsami [Gas flows with particles ]. Moscow, Fizmatlit Publ., 2008, 600 p. (In Russian)
[7] Nigmatulin R.I. Dinamika mnogofaznykh sred [Dynamics of multiphase media]. Part I. Moscow, Nauka. Fiz.-mat.lit Publ., 1987, 464 p. (In Russian)
[8] Safronov A. V. O primenimosti modeley turbulentnoy vyazkosti dlya rascheta sverkhzvukovykh struynykh techeniy [About the applicability of models of turbulent viscosity for the calculation of supersonic jet flows]. Fizikokhimicheskaya kinetika v gazovoy dinamike, 2012. vol. 13, no. 1. (In Russian)
[9] Sinilshchikov B. E., Sinilshchikov V. B., Andreev O. V. Ispol’zovaniye modeli G. N. Abramovicha dlya ucheta vliyaniya chastits na turbulentnost’ pri prikladnykh chislennykh raschetakh sverkhzvukovykh struynykh techeniy [Using the model of GN Abramovich to take into account the effect of particles on turbulence in applied numerical calculations of supersonic jet flows ]. Sb. trudov VII Mezhdunarodnoy konferentsii po neravnovesnym protsessam v soplakh i struyakh (NPNJ-2008). Moscow, 2008. (In Russian)
[10] Alemasov V. E., Dregalin A. F., Tishin A. P. Teoriya raketnykh dvigateley [The theory of rocket engines]. Edited by V. P. Glushko, Moscow, Mashinostroyeniye Publ., 1989, 464 p. (In Russian)
[11] Beletskiy Yu. M., Voynovich P. A., Il’in S. A., Timofeev E. V., Fursenko A. A. Sravnenie nekotorykh skhem skvoznogo scheta [Comparison of some cross-account schemes]. Chast’ 1. Statsionarnye techeniya, L. Preprint ITF im. A.F. Ioffe № 1383, 1989, 67 p. (In Russian)
[12] Andreev O. V., Zyuzlikov V.P., Sinilshchikov B.E., Sinilshchikov V.B., Gonchar A.G., Sokolova T.T., Shilov L.A. Sopostavleniye raschetnykh i eksperimental’nykh dannykh o vzaimodeidtvii strui s gazootrazhatelem v sluchae priosevogo vpryska vody [A comparison of the calculated and experimental data on the interaction of a jet with a gas reflector in the case of an axial injection of water]. Kosmonavtika i raketostroenie, № 3 (56), 2009, pp. 5–14. (In Russian)
For citing this article
Sinilshchikov B.E., Sinilshchikov V.B. Investigation of force and thermal loading of jet deflectors of launch complexes of space rockets during the work of water supply systems // The Research of the Science City, 2017, vol. 1, no. 2, pp. 61-71.
This Article is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License (CC BY-NC 4.0).