Calculation of Heat Transfer and Drag Coefficients for Aircraft Geometric Models
Source abstract
Abstract
A numerical model to calculate the heat transfer and resistance coefficients near the bodies of complex geometric shapes moving at high velocity is formulated. The processes of heat and mass transfer and flow around aircraft elements are considered. An algorithm for calculating heat fluxes and the heat transfer coefficient is proposed. The developed numerical technique can give an idea of the essential features of the flow, heat transfer at the end keels of the wings, and integral layouts of high-speed aircraft. An approximate mathematical model for calculating the heat transfer processes and resistance coefficients near the bodies of complex geometric shapes moving at high speed in the Earth’s atmosphere is formulated. The calculated results for convective heat transfer and friction coefficients for the X-33 and X-43 vehicles are obtained.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Radiative Heat Transfer Studies · Computational Fluid Dynamics and Aerodynamics · Gas Dynamics and Kinetic Theory
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
Thermal Physics Department, Bauman Moscow State Technical University, 105005 Moscow, Russia
Joint Institute for High Temperatures, Russian Academy of Sciences, 125412 Moscow, Russia
Funding
Ministry of Science and Higher Education of the Russian Federation “Advanced Engineering Schools” (PISh)
References (40)
Show source-provided references
1. Figliola, N., Schmidt, D., and Lee, J.-H. (2022). Pressure-and Size-Dependent Aerodynamic Drag Effects on Mach 0. 3–2.2 Microspheres for High-Precision Micro-Ballistic Characterization. Appl. Sci., 12.10.3390/app12136622 ↗
2. Wang, Z., Hu, G., Zhang, D., Kim, B., Xu, F., and Xiao, Y. (2022). Aerodynamic Characteristics of a Square Cylinder with Vertical-Axis Wind Turbines at Corners. Appl. Sci., 12.10.3390/app12073515 ↗
3. Analysis of the ideal gas flow over body of basic geometrical shape10.1016/j.ijheatmasstransfer.2018.12.032 ↗
4. DeJarnette, F., Hamilton, H.H., and Weilmuenster, K.J. (2008, January 7–10). New Method for Computing Convective Heating in Stagnation Region of Hypersonic Vehicles. Proceedings of the 46 AIAA Aerospace Sciences Meeting and Exhibit, Aerospace Sciences Meetings, AIAA 2008–1261, Reno, NV, USA.10.2514/6.2008-1261 ↗
5. Drag coefficient model to track variations due to attitude and orbital motion10.2514/1.G004854 ↗
6. Hollis, B.R., Horvath, T.J., Berry, S.A., Hamilton, H.H., and Alter, S.J. (July, January 28). X-33 Computational Aeroheating Predictions and Comparisons with Experimental Data. Proceedings of the 33rd AlAA Thermophysics Conference, AIAA 99-3559, Norfolk, VA, USA.
7. Grigoryev, Y.N., Vshivkov, V.A., and Fedoruk, M.P. (2002). Numerical-Particle-in-Cell Methods, Theory and Applications; Vandien Service Provider B.V.10.1515/9783110916706 ↗
8. Heat Transfer Measurements in an Expansion Tube Using Infrared Thermography10.2514/1.J059919 ↗
9. Churakov, D.A., Gorshkov, A.B., Kovalev, R.V., Dyadkin, A.A., and Zhurin, S.V. (2009, January 3–6). Heat Transfer of Reentry Vehicles during Atmosphere Flight. Proceedings of the European Space Agency, ESA SP 659, Versailles, France.
10. Hollis, B.R., Thompson, R.A., Murphy, K.J., Nowak, R.J., Riley, C.J., Wood, W.A., Alter, S.J., and Prabhu, R. (1999, January 9–11). X-33 Aerodynamic and Aeroheating Computations for Wind Tunnel and Flight Conditions. Proceedings of the 24th Atmospheric Flight Mechanics Conference, AIAA 99-4163, Portland, OR, USA.10.2514/6.1999-4163 ↗
11. Silvestrov, P.V., and Surzhikov, S.T. (2019). Calculation of aerothermodynamics for high-speed aircraft X-43 using computer code UST3D and UST3D-AUSMPW. Phys. Chem. Kinet. Gas Dyn., 20, Available online: http://doi.org/10.33257/PhChGD.20.4.865.10.33257/PhChGD.20.4.865 ↗
12. Numerical modeling of laser target compression in an external magnetic field10.1134/S2070048218020096 ↗
13. Surzhikov, S.T. (2003, January 8–10). Computing System for Solving Radiative Gasdynamic Problems of Entry and Re-Entry Space Vehicles. Proceedings of the 1st International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, ESA-533, Lisabon, Portugal.
14. New realization method for calculating convective heat transfer near the hypersonic aircraft surface10.1007/s00033-019-1095-1 ↗
15. Vulis, L.A. (1963). On the Overlap of Molecular and Molar Effects in the Transition Region of the Flow, Gosenergoizdat. (In Russian).
16. Gurvich, L.V., Veits, I.V., Medvedev, V.A., and Alcock, C.B. (1978). Thermodynamic Properties of Individual Substances, Nauka. (In Russian).
17. Zinin, K.M., Panasenko, A.V., and Surzhikov, S.T. (2019). Validation of computer code UST3D by the example of calculating the aerodynamic characteristics of the X-34 vehicle under various parameters. Phys. Chem. Kinet. Gas Dyn., 20, Available online: http://chemphys.edu.ru/media/published/Zinin_et_al_2019_Vol_20_No_4.pdf.10.33257/PhChGD.20.4.882 ↗
18. Calculation analysis of the experimental data of HIFiRE-1 using the computer code NERAT-2D10.1088/1742-6596/1009/1/012001 ↗
19. Some questions of differential geometry in the large
20. Andreev, S.V., Bondarev, A.E., Mikhailova, T.N., Nesterenko, A., and Ryzhova, I. (2014). Approximate Approach to Estimating Frictional Resistance on Bodies of Revolution in Viscous Flow, Keldysh Institute Preprints. (In Russian).
21. Influence of chemical kinetics and unmixedness on burning in supersonic hydrogen flames10.2514/3.50747 ↗
22. De Boor, C.A. (1978). Practical Guide to Splines, Springer.10.1007/978-1-4612-6333-3 ↗
23. Approximate convective heating analysis for hypersonic flows10.2514/3.57788 ↗
24. Hamilton, H.H., Weilmuenster, K.J., and DeJarnette, F. (2006, January 5–8). Improved Approximate Method for Computing Convective Heating on Hypersonic Vehicles Using Unstructured Grids. Proceedings of the 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference AIAA, San Francisco, CA, USA.10.2514/6.2006-3394 ↗
25. Hamilton, H.H., Weilmuenster, K.J., and DeJarnette, F. (2009, January 22–25). Approximate Method for Computing Laminar and Turbulent Convective Heating on Hypersonic Vehicles Using Unstructured Grids. Proceedings of the 41st AIAA Thermophysics Conference, San Antonio, TX, USA.10.2514/6.2009-4310 ↗
26. Approximate method for calculating convective heat flux on the surface of bodies of simple geometric shapes10.1088/1742-6596/815/1/012024 ↗
27. Martin, J., and Gliffs, N.J. (1969). Atmospheric Reentry. An Introduction to Its Science and Engineering, Prentice-Hall Inc.
28. Theory of stagnation point heat transfer in dissociated air
29. X-33 Computational Aeroheating Predictions and comparison with experimental data10.2514/2.3751 ↗
30. Approximate calculation of convective heat transfer near hypersonic aircraft surface10.1615/JEnhHeatTransf.2018026947 ↗
31. Air tornado-like vortices: Mathematical modelling10.1134/S0018151X17020201 ↗
32. Method of impact on free nonstationary air vortices10.1134/S0018151X12040219 ↗
33. Stagnation-point radiative heating relations for earth and mars entries10.2514/3.26206 ↗
34. Kuzenov, V.V., Ryzhkov, S.V., and Varaksin, A.Y. (2022). The Adaptive Composite Block-Structured Grid Calculation of the Gas-Dynamic Characteristics of an Aircraft Moving in a Gas Environment. Mathematics, 10.10.3390/math10122130 ↗
35. Two-phase boundary layer of gas with solid particles10.1134/S0018151X20050107 ↗
36. Modern approaches for calculating flow parameters during a laminar–turbulent transition in a boundary layer10.1134/S0018151X18010042 ↗
37. Analytical solution of the problem of conjugate heat transfer between a gasdynamic boundary layer and anisotropic strip
38. Khan, S., Selim, M.M., Khan, A., Ullah, A., Abdeljawad, T., Ayaz, M., and Mashwani, W.K. (2021). On the analysis of the non-newtonian fluid flow past a stretching/shrinking permeable surface with heat and mass transfer. Coatings, 11.10.3390/coatings11050566 ↗
39. Varaksin, A.Y., and Ryzhkov, S.V. (2022). Vortex Flows with Particles and Droplets (A Review). Symmetry, 14.10.3390/sym14102016 ↗
40. Numerical solutions of higher order boundary value problems via wavelet approach10.1186/s13662-021-03495-6 ↗