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Fluid Dynamics

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01-12-2022

Problems of Radiative Gas Dynamics in the Fire-II Space Experiment

Author: S. T. Surzhikov

Published in: Fluid Dynamics | Special Issue 2/2022

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Abstract

The results of a systematic numerical analysis of the experimental data of the Fire-II flight experiment and a consideration of the results of a computational study of the convective and radiative heating of the indicated experimental space experiment, taking the atomic lines of atoms and ions, using the NERAT(2D) + ASTEROID computer platform into account, are presented. The specified computer platform is designed to solve the complete system of equations of radiative gas dynamics of a viscous, thermally conductive, physically and chemically nonequilibrium gas and radiative transport in two-dimensional geometry. The spectral optical properties of high-temperature gases have been calculated using ab-initio quasi-classical and quantum mechanical methods. The calculation of the transfer of selective thermal radiation was performed using the line-by-line method on specially generated computational grids along the radiation wavelength, which makes it possible to achieve significant savings in computing resources.

previous article The Radiative Gas Dynamics of a Descent Space Capsule under Conditions of Orbital and Superorbital Entry into the Earth’s Atmosphere

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Cauchon, D.L., Radiative heating results from the Fire II flight experiment at reentry velocity of 11.4 km/s, NASA TM X-1402, 1967.

Cauchon, D.L., Mckee, C.W., and Cornette, E.S., Spectral measurements of gas-cap radiation during project Fire flight experiment at reentry velocities near 11.4 km/s, NASA TM X-1389, 1967.

Cornette, E.S., Forebody temperature and calorimeter heating rates measured during project Fire II reentry at 11.35 km/s, NASA TM X-1305, 1966.

Olynick, D.R., Henline, W.D., Hartung, L.C., and Candler, G.V., Comparison of coupled radiative flow solutions with project Fire-II flight data, J. Thermophys. Heat Transfer, 1995, vol. 9, no. 4, pp. 586–594. https://doi.org/10.2514/3.712CrossRef

Olynick, D.R., Henline, W.D., Chambers, L.H., and Candler, G.V., Comparisons of coupled radiative Navier–Stokes flow solutions with the project Fire II flight data // AIAA Paper 94-1955. 1994.

Johnston, C.O., Hollis, B.R., and Sutton, K., Spectrum modeling for air shock-layers at lunar-return conditions, J. Spacecr. Rockets, 2008, vol. 45, no. 5, pp. 865–878. https://doi.org/10.2514/1.33004ADSCrossRef

Johnston, C.O., Hollis, B.R., and Sutton, K., Non-Boltzmann modeling for air shock-layers at lunar return conditions, J. Spacecr. Rockets, 2008, vol. 45, no. 5, pp. 879–890. https://doi.org/10.2514/1.33006ADSCrossRef

Johnston, C.O., Hollis, B.R., and Sutton, K., Nonequilibrium stagnation-line radiative heating for Fire-II, J. Spacecr. Rockets, 2008, vol. 45, no. 6, pp. 1185–1195. https://doi.org/10.2514/1.33008ADSCrossRef

Candler, G.V., The computation of weakly ionized hypersonic flows in chemical nonequilibrium, PhD Dissertation, Stanford, Calif.: Stanford Univ., 1988.

10.

Hartung, L.C., Mitcheltree, R.A., and Gnoffo P.A., Coupled radiation effects in thermochemical nonequilibrium shock capturing flowfield calculation, 27th Thermophysics Conf., Nashville, Tenn., 1992, AIAA, 1992, p. 92-2868. https://doi.org/10.2514/6.1992-2868

11.

Gnoffo, P.A., Gupta, R.N., and Shinn, J.L., Conservation equations and physical models for hypersonic air flows in thermal and chemical nonequilibrium, NASA TP-2867, 1989.

12.

Candler, G.V. and MacCormack R.W., The computation of hypersonic ionized flows in chemical and thermal nonequilibrium, J. Thermophys. Heat Transfer, 1991, vol. 5, no. 3, pp. 266−273.ADSCrossRef

13.

Lee, J.H., Basic governing equations for the flight regimes of aeroassisted orbital transfer vehicles, Thermal Design of Aeroassisted Orbital Transfer Vehicles, Nelson, H.F., Progress in Astronautics and Aeronautics, vol. 96, New York: AIAA, 1985, pp. 3−53.

14.

Park, C., Review of chemical-kinetic problems of future NASA missions, I: Earth entries, J. Thermophys. Heat Transfer, 1993, vol. 15, no. 3, pp. 385–398. https://doi.org/10.2514/3.431CrossRef

15.

Park, C., Nonequilibrium Hypersonic Aerothermodynamics, New York: J. Wiley & Sons, 1990.

16.

Sutton, K., Air radiation revisited, 19th Thermophysics Conf., Snowmass, Colo., 1984, AIAA, 1984, p. 84-1733. https://doi.org/10.2514/6.1984-1733

17.

Balakrishnan, A., Park, C., and Green, M.J., Radiative viscous- shock-layer analysis of Fire, Apollo, and PAET flight data, 20th Thermophysics Conf., Williamsbrug, Va., 1985, AIAA, 1985, p. 1985-1064. https://doi.org/10.2514/6.1985-1064

18.

Gupta, R.N., Navier–Stokes and viscous shock-layer solutions for radiating hypersonic flows, 22nd Thermophysics Conf., Honolulu, Hawaii, 1987, AIAA, 1987, p. 87-1576. https://doi.org/10.2514/6.1987-1576

19.

Bird, G.A., Nonequilibrium radiation during re-entry at 10 km/s, 22 Thermophysics Conf., Honolulu, Hawaii, 1987, AIAA, 1987, p. 87-1543. https://doi.org/10.2514/6.1987-1543

20.

Carlson, L.A., Approximations for hypervelocity nonequilibrium radiating, reacting, and conducting stagnation regions, J. Thermophys. Heat Transfer, 1989, vol. 3, no. 4, pp. 380–388. https://doi.org/10.2514/3.28764ADSCrossRef

21.

Gally, T.A., Development of engineering methods for nonequilibrium radiative phenomena about aeroassisted entry vehicles, PhD Dissertation, College Station, Texas: Texas A&M Univ., 1992.

22.

Greendyke, R.B. and Hartung, L.C., Convective and radiative heat transfer analysis for the Fire II forebody, J. Spacecr. Rockets, 1994, vol. 31, no. 6, pp. 986–992. https://doi.org/10.2514/3.26548ADSCrossRef

23.

Park, C., Stagnation-point radiation for Apollo-4, J. Thermophys. Heat Transfer, 2004, vol. 18, no. 3, pp. 349–357. https://doi.org/10.2514/1.6527CrossRef

24.

Park, C., Problems of rate chemistry in the flight regimes of aeroassisted orbital transfer vehicles, 19th Thermophysics Conf., 1984, AIAA, 1984, p. 84-1730. https://doi.org/10.2514/6.1984-1730

25.

Park, C., Assessment of two-temperature kinetic model for dissociating and weakly ionizing nitrogen, J. Thermophys. Heat Transfer, 1988, vol. 2, no. 1, pp. 8–16. https://doi.org/10.2514/3.55ADSCrossRef

26.

McBride, B.J., Zehe, M.J., and Gordon, S., NASA Glenn coefficients for calculating thermodynamic properties of individual species, NASA TP 2002-211556, 2002.

27.

Hartung, L.C., Development of a nonequilibrium radiative prediction method for coupled flowfield solutions, J. Thermophys. Heat Transfer, 1992, vol. 6, no. 4, pp. 618–625. https://doi.org/10.2514/3.11542ADSCrossRef

28.

Greendyke, R.B., Parametric analysis of radiative structure in aerobrake shock layers, J. Spacecr. Rockets, 1993, vol. 30, no. 1, pp. 51–58. https://doi.org/10.2514/3.25470ADSCrossRef

29.

Sutton, K. and Gnoffo, P.A., Multi-component diffusion with application to computational aerothermodynamics, 7th AIAA/ASME Joint Thermophysics and Heat Transfer Conf., Albuquerque, N.M., 1988, AIAA, 1988, p. 98-2575. https://doi.org/10.2514/6.1998-2575

30.

Ralchenko, Yu., Jou, F.-C., Kelleher, D.E., Kramida, A.E., Musgrove, A., Reader, J., Wiese, W.L., and Olsen, K., NIST Atomic Spectra Database, Version 3.1.0. National Inst. of Standards and Technology (NIST) Physics Lab., 2006. http://physics.nist.gov/PhysRefData/ASD/index. Cited September 3, 2006.

31.

The Opacity Project, Philadelphia: Taylor, 1995, vol. 1.

32.

Cunto, W., Mendoza, C., Ochsenbein, F., and Zeippen, C. J., TOPbase at the CDS, Astron. Astrophys., 1993, vol. 275, pp. L5–L8. http://vizier.u-strasbg.fr/topbase/topbase.html. Cited September 3, 2006.ADS

33.

Soon, W.H. and Kunc, J.A., Nitrogen plasma continuum emission associated with N-(³ P) and N-(¹ D) ions, Phys. Rev. A, 1990, vol. 41, no. 8, pp. 4531–4533. https://doi.org/10.1103/PhysRevA.41.4531ADSCrossRef

34.

Chauveau, S., Deron, C., Perrin, M.-Y., Rivière, Ph., and Soufiani, A., Radiative transfer in LTE air plasmas for temperatures up to 15,000K, J. Quant. Spectrosc. Radiat. Transfer, 2003, vol. 77, no. 2, pp. 113–130. https://doi.org/10.1016/S0022-4073(02)00080-8ADSCrossRef

35.

Chambers, L.H., Predicting radiative heat transfer in thermochemical nonequilibrium flow fields, NASA TM-4564, 1994.

36.

Laux, C.O., Optical diagnostics and radiative emission of air plasmas, Rept. T-288, Stanford, Calif.: High Temperature Gas Dynamics Lab., Mechanical Engineering Dept., Stanford Univ., 1993.

37.

Whang, T.J., Guoxing, Z., Stwalley, W.C., and Wu, C.Y.R., Franck–Condon factors of the transitions of N₂, J. Quant. Spectrosc. Radiat. Transfer, 1996, vol. 55, no. 3, pp. 335–344. https://doi.org/10.1016/0022-4073(95)00169-7ADSCrossRef

38.

Stahel, D., Leoni, M., and Dresslar, K., Nonadiabatic representations of the ¹Σ⁺ _u and ¹Π_u states of the N₂ molecule, J. Chem. Phys., 1983, vol. 79, no. 6, pp. 2541–2558. https://doi.org/10.1063/1.446166ADSCrossRef

39.

Chauveau, S., Perrin, M.-Y., Rivière, Ph., and Soufiani, A., Contributions of diatomic molecular electronic systems to heated air radiation, J. Quant. Spectrosc. Radiat. Transfer, 2002, vol. 72, no. 4, pp. 503–530. https://doi.org/10.1016/S0022-4073(01)00141-8ADSCrossRef

40.

Park, C., Radiation enhancement by nonequilibrium in Earth’s atmosphere, J. Spacecr. Rockets, 1985, vol. 22, no. 1, pp. 27–36. https://doi.org/10.2514/3.25706ADSCrossRef

41.

Surzhikov, S.T., Radiatsionnaya gazovaya dimanika spuskaemykh kosmicheskikh apparatov. Mnogotemperaturnye modeli (Radiative Gas Dynamics of Space Capsules: Multitemperature Models), Moscow: Inst. Probl. Mekhaniki Ross. Akad. Nauk, 2013.

42.

Surzhikov, S.T., Opticheskie svoistva gazov i plazmy (Optical Properties of Gases and Plasma), Moscow: Izd-vo Mosk. Gos. Tekh. Univ. im. N.E. Baumana, 2004.

43.

Edwards, J.R. and Liou, M.-S., Low-diffusion flux-splitting methods for flows at all speeds, AIAA J., 1998, vol. 36, no. 9, pp. 1610–1617. https://doi.org/10.2514/2.587ADSCrossRef

44.

Surzhikov, S.T., Analytical methods of constructing finite-differences grids for computing aerothermodynamics of space capsules, Vestn. Mosk. Gos. Tekh. Univ. N.E. Baumana, 2004, no. 2, pp. 24–50.

45.

Surzhikov, S.T., A study of the influence of kinetic models on calculations of the radiation-convective heating of a space vehicle in Fire-II flight experiment, Russ. J. Phys. Chem. B, 2008, vol. 2, no. 5, pp. 814–826. https://doi.org/10.1134/S1990793108050254CrossRef

46.

Dunn, M.G. and Kang, S.W., Theoretical and experimental studies of reentry plasmas, NASA CR 2232, 1973.

47.

Thermodynamic Properties of Individual Substances, vol. 1: Elements O, H(D, T), F, Cl, Br, I, He, Ne, Ar, Kr, Xe, Rn, S, N, P, and Their Compounds, part 1: Methods and Computation, Gurvich, L.V., Veyts, I.V., Alcock, C.B., and Iorish, V.S., Eds., Hemisphere Publishing Corporation, 1989, 4th ed.

48.

Chase, M.W., Davies, C.A., Downey, J.R., Jr., Frurip, D.J., McDonald, R.A., and Syvertud, A.N., JANAF thermochemical tables. Third edition. I: Al–Co, J. Phys. Chem. Ref. Data, 1985, vol. 14, no. 1.

49.

Chase, M.W., Davies, C.A., Downey, J.R., Jr., Frurip, D.J., McDonald, R.A., and Syvertud, A.N., JANAF thermochemical tables: Third edition. II: Cr–Zr, J. Phys. Chem. Ref. Data, 1985, vol. 14, pp. 927–1856.

50.

Bates, D.R. and Damgaard, A., The calculation of the absolute strengths of spectral lines, Philos. Trans. R. Soc. A, 1949, vol. 242, pp. 101–122. https://doi.org/10.1098/rsta.1949.0006ADSCrossRefMATH

51.

Sobel’man, I.I., Vvedenie v teoriyu atomnykh spektrov (Introduction to the Theory of Atomic Specra), Moscow: Gos. Izd-vo Fiz.-Mat. Literatury, 1963.

52.

Treanor, C.E. and Marrone, P.V., Effect of dissociation on the rate of vibrational relaxation, Phys. Fluids, 1962, vol. 5, no. 9, pp. 1022–1026. https://doi.org/10.1063/1.1724467ADSCrossRef

53.

Surzhikov, S.T., Vychislitel’nyi eksperiment v postroenii radiatsionnykh modelei mekhaniki izluchayushchego gaza (Computational Experiment in Constructing Radiation Models of Mechanics of Radiative Gas), Moscow: Nauka, 1992.

54.

Bartlett, E.P., Kendal, R.M., and Rindal, R.A., An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator: Part IV-A Unified Approximation for Mixture Transport Properties for Multicomponent Boundary-Layer Applications. NASA CR-1063. 1968.

55.

Gekcen, T., Computation of Nonequilibrium Radiating Shock Layers. AIAA Paper 93-0144. 1993.

56.

Hash, D., Olejniczak, J., Wright, M., Prabhu, D., Pulsonetti, M., Hollis, B., Gnoffo, P., Barhardt, M., Nompelis, I., Candler, G. Fire-II Calculations for Hypersonic Nonequilibrium Aerothermodynamics Code Verification: DPLR, LAURA, and US3D. AIAA Paper 2007-0605. 2007.

57.

Surzhikov, S.T., The Role of the Spectral Lines of Atoms and Ions in Radiative Heating of the Surfaces of Space Capsules. Fluid Dyn., 2022, Vol. 23, Suppl. 2.

Title: Problems of Radiative Gas Dynamics in the Fire-II Space Experiment
Author: S. T. Surzhikov
Publication date: 01-12-2022
Publisher: Pleiades Publishing
Published in: Fluid Dynamics / Issue Special Issue 2/2022
Print ISSN: 0015-4628
Electronic ISSN: 1573-8507
DOI: https://doi.org/10.1134/S0015462822100676

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