Email this article 
Complex approach to aerodynamic design of inlet ducts with submerged vortex-free air intakes
- Authors: Kornev A.V.1, Boychuk I.P.2
-
Affiliations:
- Zhukovski National Aerospace University “Kharkov Aviation Institute”
- Belgorod State Technological University named after V.G. Shoukhov
- Issue: Vol 16, No 2 (2017)
- Pages: 47-59
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/5118
- DOI: https://doi.org/10.18287/2541-7533-2017-16-2-47-59
- ID: 5118
Cite item
Full Text
Abstract
The paper shows the possibility of improving gas-dynamic characteristics of a submerged air intake and presents a technology of developing design solutions according to the principle of conformity to the flow lines. The gas-dynamic principle of shaping is provided by means of computer-aided integrated technologies of design and application of numerical visualization methods as design tools. The revealed regularity of the working process of the external streamline of the preceding airframe surfaces unambiguously defines the fundamental design distinctions of the conformal air intake in the form of the converging side edges on the stream and determines its advantages over the analogs.
About the authors
A. V. Kornev
Zhukovski National Aerospace University “Kharkov Aviation Institute”
Author for correspondence.
Email: koral.v15@gmail.com
senior research scientist, Research and Development Institute of problems of physical modeling of aircraft flight modes
Russian FederationI. P. Boychuk
Belgorod State Technological University named after V.G. Shoukhov
Email: ip.boychuk@gmail.com
Candidate of Science (Engineering)
Associate Professor, Department of Computer Software and Automated Systems
References
- Kornev A.V. Aspects of creating an efficient power plant with submerged air intake with outer vortex generators. Systems of Arms and Military Equipment. 2012. No. 3 (31). P. 167-180. (In Russ.)
- Ferguson S.D., Eastman D.W. High performance submerged airinlet. Patent US, no. 4378097, 1980 (Publ. 29.03.1983).
- Rolls L.S. A flight comparison of a submerged inlet and a scoop inlet at transonic speeds. NACA RM №A53A06. Washington: Langley, 1953. 42 p.
- Kornev O.V. Lіtal'niy aparat z verkhn'oroztashovanim vkhіdnim pristroєm [Aircraft with top-mounted air inlet]. Patent Ukraine, no. 103196, 2007 (Publ. 25.09.2013, bul. no. 18).
- Taskinoglu E.S., Knight D.D. Design optimization for submerged inlets. Part I. 41st Aerospace Sciences Meeting and Exhibit. Reno, Nevada, 2003. doi: 10.2514/6.2003-1247
- Akman O. Subsonic-transonic submerged intake design for a cruise missile. Diss. master of science in aerospace engineering. Ankara, 2014. 99 p.
- Harris C.D. NASA supercritical airfoils. A matrix of family-related airfoils. NASA technical paper 2969. Hampton, Virginia: Langly Research Center, 1990. 72 p.
- Shepshelovich M., Steinbuch M. Hybrid transonic-subsonic aerofoils. Patent US, no. 8186616 B2, 2012 (Publ. 29.05.2012).
- Boychuk I.P. Metod kompleksnogo aerodinamicheskogo modelirovaniya svobodno letayushchey modeli «planer-dvigatel'». Avtoreferat diss. kand. tekhn. nauk [Method of complex aerodynamic modeling of a freely flying “airframe-engine” system. Extended abstract of Cand. Sci. (Eng.) Dissertation]. Kharkov, 2012. 21 p.
- Ambroźewicz M.V., Kornev A.V., Sereda V.A. A low resource submodel of turbojet engine. Aviatsionno-kosmicheskaya tekhnika i tekhnologiya. 2016. No. 1 (128). P. 44-52. (In Russ.)
- Druzhinin E.D., Chmovzh V.V., Kornev A.V. Application of aerodynamic design methods while life cycle implementation for advanced aeronautical engineering development. Systems of Arms and Military Equipment. 2011. No. 4 (28). P. 48-57. (In Russ.)
- Polikovskiy V.I. Samoletnye silovye ustanovki [Aircraft power plants]. Moscow: Oborongiz Publ., 1952. 600 p.
- Küchemann D., Weber J. Aerodynamics of Propulsion. New York: McGraw Hill, 1953. 340 p.
- Devnin S.I. Aerogidromekhanika plokhoobtekaemykh konstruktsiy. Spravochnik [Aero hydrodynamics of high-drag bodies]. Leningrad: Sudostroenie Publ., 1983. 332 p.
Supplementary files
