Integrated approach to gas-dynamic designing of supersonic air intakes of aircraft
Abstract
The analytical and experimental studies of the aircraft’s supersonic air intakes have been carried out. An integrated approach to the gas-dynamic designing of aircraft’s supersonic air intakes that eliminates the scale effect problem of a wind tunnel with a small-sized testing area is proposed. The designing approach accelerates the development process and reduces the resource intensity due to the rational distribution of tasks between numerical and physical experiments. The results of the unique tests of the scaled ramjet’s air intake physical model in the supersonic wind tunnel are presented.
Keyword : integrated approach, supersonic air intake, scale effect, similarity criteria, numerical experiment, physical experiment
How to Cite
Kornev, A., Stetsenko, S., Yatsenko, V., Smolyakov, A., & Kalinichenko, D. (2021). Integrated approach to gas-dynamic designing of supersonic air intakes of aircraft. Aviation, 25(1), 1-9. https://doi.org/10.3846/aviation.2021.12327
This work is licensed under a Creative Commons Attribution 4.0 International License.
References
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Rademakers, R., Bindl, S., Brehm, S., Muth, B., & Niehuis, R. (2013). Investigation of flow distortion in an integrated inlet of a jet engine. In 62nd German Aerospace Congress, Conference Paper D-85577. Stuttgart, September 2013. https://www.researchgate.net/publication/257014200_Investigation_of_Flow_Distortion_in_an_Integrated_Inlet_of_a_Jet_Engine
Bedretdinov, I. (2005). The strike and reconnaissance aircraft T-4 (Volume 2). Series “The Golden Fund of Domestic Aviation” (248 p.). “Bedretdinov and Co. Publishing Group” LLC.
Davis, M. W., Jr., Hale, A. A., Klepper, J., Dubreus, T., & Cousins, W. T. (2010, 4–7 January). Demonstration of an Integrated Test and Evaluation (IT&E) process for airframe-propulsion systems as applied to a current weapon system program. In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2010 –1039. Orlando, Florida. https://doi.org/10.2514/6.2010-1039
Druzhinin, E. A., Chmovzh, V. V., & Kornev, A. V. (2011). Application of aerodynamic design methods while life cycle implementation for advanced aeronotical engineering development. Science magazine “Weapons systems and military equipment”, 4(28), 48–57.
Dubov, B. S., & Maskaev, V. K. (1983). Metrological support of instrumentation for measuring pressure in wind tunnels. In Proceedings of TsAGI, TsAGI, 227, 40–52. Moscow. http://www.hups.mil.gov.ua/periodic-app/article/1906/soivt_2011_4_12.pdf
DTIC. (1991). Air intakes for high speed vehicles.In Report documentation page AGARD-AR-270. Neuilly sur Seine: AGARD NATO, sept. 1991 (pp. 183–211). https://archive.org/details/DTIC_ADA248270/page/n61
Holland, S. D. (1991). Computational and experimental investigation of a Three-Dimensional Hypersonic Scramjet Inlet Flow Field (676 p.) [PhD thesis in aerospace engineering, hypersonic aerodynamics. North Carolina State University].
Jirasek, А. (2007, 20–21 June). Example of integrated CFD and experimental studies: design of flow control in the FOIEIC-01 Inlet. In 3rd International Symposium on Integrating CFD and Experiments in Aerodynamics. U.S. Air Force Academy. http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.556.6504&rep=rep1&type=pdf
Karpov, E. V., & Novogorodtsev, E. V. (2014a, 22–24 April). Calculation of flow in trapezoidal air intake with the curvilinear channel. In Collected theses of the reports of the scientific-practical conference “Innovations in Aviation and Cosmonautics–2014” (pp. 51–52). MAI. https://docplayer.ru/36051430-Innovacii-v-aviacii-i-kosmonavtike-2014.html
Karpov, E. V., & Novogorodtsev, E. V. (2014b, 17–21 November). Numerical investigation of the boundary-layer suction effect on capability of trapezoidal air inlet. In Collected theses of the reports of the 13th International Conference “Aviation and Cosmonautics–2014” (pp. 64–65). MAI. http://files.mai.ru/site/conf/aik/2014/Abstracts.pdf
Karpova, V. E., & Meshennikov, P. A. (2014, 22–24 April). Computational research of a frontal air intake device for smallsized high-speed aircraft. In Collected theses of the reports of the scientific-practical conference “Innovations in Aviation and Cosmonautics–2014” (p. 30). MAI. http://files.mai.ru/site/conf/aik/2014/Abstracts.pdfhttps://docplayer.ru/36051430-Innovacii-v-aviacii-i-kosmonavtike-2014.html
Knight, D. (2003, 3 June). Data driven design optimization methodology a dynamic data driven application system. In International Conference on Computational Science, Paper (p. 29). ICCS03. http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.121.1409&rep=rep1&type=pdf
Kornev, A. V., & Boychuk, I. P. (2017). Complex approach to aerodynamic design of inlet ducts with submerged vortexfree air intakes. Bulletin of the Samara University. Aerospace Technics, Technologies and Mechanical Engineering, 16(2), 47–59. Samara National Research University named after academician S.P. Korolev. http://journals.ssau.ru/index.php/vestnik/article/view/5118
Kornev, A. V., Sereda, V. A., & Migalin, K. V. (2018). Aerodynamic design method of integrated aircraft with submerged intake devices and power plant included into airframe carrying system. Russian Aeronautics, 61(1), 17–25. https://link.springer.com/article/10.3103%2FS1068799818010038
Petunin, A. N. (1986). Errors of measurement of the main parameters of subsonic and supersonic flow with various combinations of partial errors of pressure measurement. In Proceedings of TsAGI, 1024, 39–76. TsAGI.
Rademakers, R., Bindl, S., Brehm, S., Muth, B., & Niehuis, R. (2013). Investigation of flow distortion in an integrated inlet of a jet engine. In 62nd German Aerospace Congress, Conference Paper D-85577. Stuttgart, September 2013. https://www.researchgate.net/publication/257014200_Investigation_of_Flow_Distortion_in_an_Integrated_Inlet_of_a_Jet_Engine