Aerothermal Heating Correlations at Stagnation Point/Line in Low-Enthalpy Hypersonic Flow

No AccessTechnical NotesAerothermal Heating Correlations at Stagnation Point/Line in Low-Enthalpy Hypersonic FlowBingkang Zhou, Xiangyu Yi, Zhaowei Wang and Zhufei LiBingkang ZhouUniversity of Science and Technology of China, 230027 Hefei, People’s Republic of China*Ph.D. Student, Department of Modern Mechanics.Search for more papers by this author, Xiangyu YiChina Academy of Aerospace Aerodynamics, 100074 Beijing, People’s Republic of China†Senior Engineer.Search for more papers by this author, Zhaowei WangChina Academy of Launch Vehicle Technology, 100076 Beijing, People’s Republic of China‡Researcher.Search for more papers by this author and Zhufei LiUniversity of Science and Technology of China, 230027 Hefei, People’s Republic of China§Associate Professor, Department of Modern Mechanics; (Corresponding Author).Search for more papers by this authorPublished Online:3 Jan 2023https://doi.org/10.2514/1.J062455SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Bertin J. J. and Cummings R. M., “Critical Hypersonic Aerothermodynamic Phenomena,” Annual Review of Fluid Mechanics, Vol. 38, Jan. 2006, pp. 129–157. https://doi.org/10.1146/annurev.fluid.38.050304.092041 CrossrefGoogle Scholar[2] Li Z., Zhang Z., Wang J. and Yang J., “Pressure-Heat Flux Correlations for Shock Interactions on V-Shaped Blunt Leading Edges,” AIAA Journal, Vol. 56, No. 1, 2019, pp. 356–367. https://doi.org/10.2514/1.J058538 Google Scholar[3] Xiao F., Li Z., Zhang Z., Zhu Y. and Yang J., “Hypersonic Shock Wave Interactions on a V-Shaped Blunt Leading Edge,” AIAA Journal, Vol. 56, No. 1, 2018, pp. 356–367. https://doi.org/10.2514/1.J055915 LinkGoogle Scholar[4] Zhang Z., Li Z. and Yang J., “Transitions of Shock Interactions on V-Shaped Blunt Leading Edges,” Journal of Fluid Mechanics, Vol. 912, April 2021, Paper A12. https://doi.org/10.1017/jfm.2020.1117 Google Scholar[5] Anderson J. D., Hypersonic and High-Temperature Gas Dynamics, 2nd ed., AIAA, Reston, VA, 2006, pp. 261–374. https://doi.org/10.2514/4.861956 LinkGoogle Scholar[6] Bertin J. J., Hypersonic Aerothermodynamics, AIAA, Washington, D.C., 1994, pp. 231–276. https://doi.org/10.2514/4.470363 Google Scholar[7] Park S. H., Neeb D., Plyushchev G., Leyland P. and Gülhan A., “A Study on Heat Flux Predictions for Re-Entry Flight Analysis,” Acta Astronautica, Vol. 187, Oct. 2021, pp. 271–280. https://doi.org/10.1016/j.actaastro.2021.06.025 CrossrefGoogle Scholar[8] Tauber M. E., “A Review of High-Speed, Convective, Heat-Transfer Computation Methods,” NASA TP-2914, 1989. Google Scholar[9] West T. K. and Brandis A. M., “Stagnation-Point Aeroheating Correlations for Mars Entry,” Journal of Spacecraft and Rockets, Vol. 57, No. 2, 2020, pp. 319–327. https://doi.org/10.2514/1.A34602 LinkGoogle Scholar[10] Van Driest E. R., “The Problem of Aerodynamic Heating,” Aeronautical Engineering Review, Vol. 15, No. 10, 1956, pp. 26–41. Google Scholar[11] Fay J. A. and Riddell F. R., “Theory of Stagnation Point Heat Transfer in Dissociated Air,” Journal of the Aerospace Sciences, Vol. 25, No. 2, 1958, pp. 73–85. https://doi.org/10.2514/8.7517 LinkGoogle Scholar[12] Scala S. M., A Study of Hypersonic Ablation, Springer, Berlin, 1960, pp. 790–827. https://doi.org/10.1007/978-3-662-39914-9_67 Google Scholar[13] Lees L., “Laminar Heat Transfer over Blunt-Nosed Bodies at Hypersonic Flight Speeds,” Journal of Jet Propulsion, Vol. 26, No. 4, 1956, pp. 259–269. https://doi.org/10.2514/8.6977 LinkGoogle Scholar[14] Detra R. W., Kemp N. H. and Riddell F. R., “Addendum to ‘Heat Transfer to Satellite Vehicles Re-Entering the Atmosphere’,” Journal of Jet Propulsion, Vol. 27, No. 12, 1957, pp. 1256–1257. Google Scholar[15] Sutton K. and Graves R. A., “A General Stagnation-Point Convective Heating Equation for Arbitrary Gas Mixtures,” NASA TR-R-376, 1971. Google Scholar[16] Bushnell D. M., “Scaling: Wind Tunnel to Flight,” Annual Review of Fluid Mechanics, Vol. 38, Jan. 2006, pp. 111–128. https://doi.org/10.1146/annurev.fluid.38.050304.092208 CrossrefGoogle Scholar[17] Simeonides G., “Generalized Reference Enthalpy Formulations and Simulation of Viscous Effects in Hypersonic Flow,” Shock Waves, Vol. 8, No. 3, 1998, pp. 161–172. https://doi.org/10.1007/s001930050109 CrossrefGoogle Scholar[18] Wen C., “Hypervelocity Flow over Spheres,” Ph.D. Dissertation, California Inst. of Technology, Pasadena, CA, 1994. Google Scholar[19] Hollis B. R., “Blunt-Body Entry Vehicle Aerothermodynamics: Transition and Turbulence on the CEV and MSL Configurations,” AIAA Paper 2010-4984, 2010. https://doi.org/10.2514/6.2010-4984 Google Scholar[20] Du T., Chen M. K., Li H. L., Zhang Y. L. and Shen D., “Suitability Analysis on Correlation Relation of Aerothermodynamics Entry Environment for Hypersonic Flying Vehicles,” Journal of Astronautics, Vol. 39, No. 9, 2018, pp. 1039–1046. https://doi.org/10.3873/j.issn.1000-1328.2018.09.012 Google Scholar[21] Holden M. S. and Kolly J. M., “Attachment Line Transition Studies on Swept Cylindrical Leading Edges at Mach Numbers from 10 to 12,” AIAA Paper 1995-2279, 1995. https://doi.org/10.2514/6.1995-2279 LinkGoogle Scholar[22] Bushnell D. M., “Interference Heating on a Swept Cylinder in Region of Intersection with a Wedge at Mach Number 8,” NASA TN-D-3094, 1965. Google Scholar[23] Poll D. I. A., “Development of Intermittent Turbulence on a Swept Attachment Line Including the Effects of Compressibility,” Aeronautical Quarterly, Vol. 34, No. 1, 1983, pp. 1–23. https://doi.org/10.1017/s0001925900009562 CrossrefGoogle Scholar[24] Beckwith I. E. and Gallagher J. J., “Local Heat Transfer and Recovery Temperatures on a Yawed Cylinder at a Mach Number of 4.15 and High Reynolds Numbers,” NASA TR R-104, 1961. Google Scholar[25] Engel C. D., “MINIVER Upgrade for the AVID System Volume 1: LANMIN User’s Manual,” NASA CR-172212, 1983. Google Scholar[26] Sharan N. and Bellan J., “Numerical Aspects for Physically Accurate Direct Numerical Simulations of Turbulent Jets,” AIAA Paper 2019-2011, 2019. https://doi.org/10.2514/6.2019-2011 Google Scholar[27] Zucrow M. J. and Hoffman J. D., Gas Dynamics, Vol. 1, Wiley, New York, 1976, pp. 160–242. Google Scholar[28] Wegener P. P. and Mack L. M., “Condensation in Supersonic and Hypersonic Wind Tunnels,” Advances in Applied Mechanics, Vol. 5, No. C, 1958, pp. 307–447. https://doi.org/10.1016/S0065-2156(08)70022-X Google Scholar[29] Tsien H. S., “Superaerodynamics, Mechanics of Rarefied Gases.” Journal of Aeronautical Sciences, Vol. 13, No. 12, 1946, pp. 653–664. https://doi.org/10.2514/8.11476 LinkGoogle Scholar[30] Borovoi V. Y., Chinilov A. Y., Gusev V. N., Struminskaya I. V., Délery J. and Chanetz B., “Interference Between a Cylindrical Bow Shock and a Plane Oblique Shock,” AIAA Paper 1996-2046, 1996. https://doi.org/10.2514/6.1996-2046 Google Scholar[31] Reijasse P., Bur R. and Chanetz B., “Experimental Analysis of Aerodynamic Interactions Occurring on Hypersonic Spacecraft,” Journal of Spacecraft and Rockets, Vol. 38, No. 2, 2001, pp. 129–135. https://doi.org/10.2514/2.3669 LinkGoogle Scholar[32] Li Z., Gao W., Jiang H. and Yang J., “Unsteady Behaviors of a Hypersonic Inlet Caused by Throttling in Shock Tunnel,” AIAA Journal, Vol. 51, No. 10, 2013, pp. 2485–2492. https://doi.org/10.2514/1.j052384 LinkGoogle Scholar[33] Chen X., Song K., Shen J. and Yi X., “The Aerodynamic and Structural Design of the Moderate Mass Piston Used in a Large Scale Hypersonic Gun Tunnel FD-20a,” Proceedings of the 32nd International Symposium on Shock Waves, Research Publishing, Singapore, 2019, pp. 1201–1207. https://doi.org/10.3850/978-981-11-2730-4_0437-cd Google Scholar[34] Liu M., Han G. and Jiang Z., “Experimental Study on the Evolution of Mode Waves in Laminar Boundary Layer on a Large-Scale Flat Plate,” Physics of Fluids, Vol. 34, No. 1, 2022, Paper 013612. https://doi.org/10.1063/5.0075710 Google Scholar[35] Nowak R. J., Hoiden M. S. and Wieting A. R., “Shock/Shock Interference on a Transpiration Cooled Hemispherical Model,” AIAA Paper 1990-1643, 1990. https://doi.org/10.2514/6.1990-1643 LinkGoogle Scholar[36] Gertsbakh I., Measurement Theory for Engineers, Springer, Berlin, 2003, pp. 88–90. https://doi.org/10.1007/978-3-662-08583-7 Google Scholar[37] Perini L. L., “Compilation and Correlation of Experimental, Hypersonic, Stagnation Point Convective Heating Rates,” Applied Physics Lab., Johns Hopkins Univ. Rept. ANSP-M-4, Silver Spring, MD, 1972. Google Scholar Previous article Next article FiguresReferencesRelatedDetails What's Popular Volume 61, Number 3March 2023 CrossmarkInformationCopyright © 2022 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc. with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsAerospace SciencesBoundary LayersEnthalpyFlow RegimesFluid DynamicsHeat ConductionHeat TransferIdeal GasThermodynamic PropertiesThermodynamicsThermophysics and Heat TransferVortex DynamicsWind Tunnels KeywordsStagnation PointHypersonic FlowsStatic EnthalpyFreestream Mach NumberWind TunnelsBoundary Layer EquationsWall TemperatureGas ConstantStagnation RegionAcknowledgmentsThis work was supported by the National Natural Science Foundation of China (grant nos. 12172354, 11772325, and 11621202). The authors are very grateful to Jiming Yang for the valuable discussions.PDF Received17 September 2022Accepted13 December 2022Published online3 January 2023