Research progress on ultraviolet radiation characteristics of hypersonic vehicles

YUAN Linhui; WANG Yu; SUN Xiaoyi

doi:10.7638/kqdlxxb-2023.0192

English Version Journal Login

您当前的位置：

首页 >

文章列表页 >

Research progress on ultraviolet radiation characteristics of hypersonic vehicles

更新时间：2026-05-28

- Research progress on ultraviolet radiation characteristics of hypersonic vehicles
- Vol. 42, Issue 10, Pages: 1-18(2024)
- 作者机构：
  
  南京工业大学城市建设学院,南京,211816
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2023.0192
  CLC： V211.4;P422.6
- Published：2024
- 稿件说明：
移动端阅览
袁琳慧, 王瑜, 孙笑一. 高速飞行器紫外辐射特性研究进展[J]. 空气动力学学报, 2024, 42(10): 1−18.

YUAN Linhui, WANG Yu, SUN Xiaoyi. Research progress on ultraviolet radiation characteristics of hypersonic vehicles[J]. 2024, 42(10): 1-18.
袁琳慧, 王瑜, 孙笑一. 高速飞行器紫外辐射特性研究进展[J]. 空气动力学学报, 2024, 42(10): 1−18. DOI： 10.7638/kqdlxxb-2023.0192

YUAN Linhui, WANG Yu, SUN Xiaoyi. Research progress on ultraviolet radiation characteristics of hypersonic vehicles[J]. 2024, 42(10): 1-18. DOI： 10.7638/kqdlxxb-2023.0192.

摘要

为了进一步明晰高速飞行器紫外辐射的相关机理与计算方法、辐射特性和未来研究方向，基于高速非平衡流场理论和紫外辐射跃迁机理，详细分析了光谱吸收系数、分子数密度等参数的计算过程，以及逐线计算法和辐射传输方程的应用场景。目前主要是通过模拟和实验手段对NO和OH分子的碰撞–辐射模型进行研究，以预测紫外光谱和辐射特性。此外，本文还综述了紫外辐射传输建模现状，明确了高速飞行器不同位置、观测角度以及飞行高度和速度对紫外辐射亮度的影响，并指出不同比例的紫外辐射源也会对飞行器尾焰的紫外辐射特性产生影响。通过对近几十年的地面和飞行实验进行研究，分析实验数据与模拟结果的差异，提出模型中可能存在的问题和不足。未来工作将集中于构建一体化辐射模型、发展先进紫外测试技术并拓展非平衡诊断技术，以满足目标特性探测和热防护系统优化等实际需求。

Abstract

This study first delves into computational methods

radiation characteristics

and underlying mechanisms of ultraviolet radiation emitted by hypersonic vehicles

the study of which holds immense significance for ensuring safe flight. Based on the principles of hypersonic non-equilibrium flows and the transition mechanisms of ultraviolet radiation

a comprehensive analysis is provided on the computational procedures for determining parameters like the spectral absorption coefficient and molecular number density. Furthermore

the study explores the application scenarios of the line-by-line calculation method and the radiative transfer equation. Numerical and experimental investigations using collision-radiation models on the ultraviolet spectral and radiation characteristics of NO and OH molecules are summarized . The current status of ultraviolet radiation transmission modeling is also presented

focusing on the influence of geometry configuration

observation angle

flight altitude

and flight speed on the ultraviolet radiation. The deficiencies of these models are identified by comparing simulation results with those obtained by recent ground and flight experiments. Future research should prioritize the development of an integrated radiation model and advanced ultraviolet testing and non-equilibrium diagnostic techniques to meet practical needs such as target characteristic detection and thermal protection system optimization.

关键词

Keywords

references

BAHM C, BAUMANN E, MARTIN J, et al. The X-43A Hyper-X Mach 7 flight 2 guidance, navigation, and control overview and flight test results[C]// AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference, Capua, Italy. Reston, Virginia: AIAA, 2005.

MERCIER R, RONALD T. Hypersonic technology (HyTech) program overview[C]// 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Norfolk, VA, USA. Reston, Virginia: AIAA, 1998.

LAU K, WOO Y, TRAN J, et al. The aerothermal, thermal and structural design process and criteria for the HIFiRE-4 flight test vehicle[C]// 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France. Reston, Virginia: AIAA, 2012.

THOMPSON R. Three-dimensional viscous-shock-layer applications for the space shuttle orbiter[C]//23rd Aerospace Sciences Meeting, Reno, NV, USA. Reston, Virginia: AIAA, 1985: AIAA1985-246.

CHEN C. Analysis of infrared radiation characteristics of hypersonic vehicle[D]. Nanjing: Nanjing University of Science and Technology, 2013 (in Chinese).

HE Z W. Research on the ultraviolet spectral radiation characteristics of atmospheric background[D]. Chengdu: University of Electronic Science and Technology of China, 2013 (in Chinese).

ZENG Y, LU L G, ZHANG B Z. Acquisition methods for ultraviolet atmospheric transmittance at astronomical sites[J]. Scientia Sinica (Physica, Mechanica Astronomica), 2022, 52(8): 132−143 (in Chinese).

KOLB C E, RYALI S B, WORMHOUDT J C. The chemical physics of ultraviolet rocket plume signatures[C]//1988 Technical Symposium on Optics, Electro-Optics, and Sensors. Proc SPIE 0932, Ultraviolet Technology II, Orlando, FL, USA. 1988, 0932: 2−23.

ABE S, FUJITA K, KAKINAMI Y, et al . Near-ultraviolet and visible spectroscopy of HAYABUSA spacecraft re-entry[J ] . Publications of the Astronomical Society of Japan, 2011 , 63 ( 5 ): 1011 − 1021 .

FUJITA K, YAMAMOTO M-Y, ABE S, et al . An overview of JAXA’s ground-observation activities for HAYABUSA reentry[J ] . Publications of the Astronomical Society of Japan, 2011 , 63 ( 5 ): 961 − 969 .

ERDMAN P W, ZIPF E C, ESPY P, et al . Flight measurements of low-velocity bow shock ultraviolet radiation[J ] . Journal of Thermophysics and Heat Transfer, 1993 , 7 ( 1 ): 37 − 41 .

ERDMAN P W, ZIPF E C, ESPY P, et al. Measurements of ultraviolet radiation from a 5 km/s bow shock[J]. Journal of Thermophysics and Heat Transfer, 1994, 8(3): 441−446.

GIZA R H, ACEVEDO P A, BLISS J D. Ultraviolet scene simulation for missile approach warning system testing[C]// Proc SPIE 3084, Technologies for Synthetic Environments: Hardware-in-the-Loop Testing II, Orlando, FL, USA, 1997.

BLANC A, DEIMLING L, EISENREICH N . UV and IR-Signatures of rocket plumes[J ] . Propellants, Explosives, Pyrotechnics: An International Journal Dealing with Scientific and Technological Aspects of Energetic Materials, 2002 , 27 ( 3 ): 185 − 189 .

PARK C . Assessment of two-temperature kinetic model for ionizing air[J ] . Journal of Thermophysics and Heat Transfer, 1989 , 3 ( 19 ): 233 − 244 .

GRASSO F, CAPANO G . Modeling of ionizing hypersonic flows in nonequilibrium[J ] . Journal of Spacecraft and Rockets, 1995 , 32 ( 2 ): 217 − 224 .

HASSAN B, CANDLER G V, OLYNICK D R . Thermo-chemical nonequilibrium effects on the aerothermodynamics of aerobraking vehicles[J ] . Journal of Spacecraft and Rockets, 1993 , 30 ( 6 ): 647 − 655 .

HU L F. Simulation of non-equilibrium flow around high-speed aircraft and optical radiation characteristics[D]. Harbin: Harbin Institute of Technology, 2011 (in Chinese).

ROBLIN A, BAUDOUX P E, CHERVET P. UV missile-plume signature model[C]// Targets and Backgrounds Ⅷ: Characterization and Representation, Orlando, 2002: 344−355.

LYU Q. Analysis of ultraviolet radiation spectrum characteristics of mixed components[D]. Xi′an: Xidian University, 2021 (in Chinese).

DONG S K, TAN H P, HE Z H, et al . Calculation of spectral absorption coefficient of high temperature equilibrium or non-equilibrium 11-species air[J ] . Chinese Journal of Aeronautics, 2001 , 14 ( 3 ): 140 − 146 .

PARK C. Calculation of nonequilibrium radiation in the flight regimes of aeroassisted orbital transfer vehicles[C]//22nd Aerospace Sciences Meeting, Reno, NV, USA. Reston, Virginia: AIAA, 1984.

ARNOLD J O, WHITING E E, LYLE G C . Line by line calculation of spectra from diatomic molecules and atoms assuming a Voigt line profile[J ] . Journal of Quantitative Spectroscopy and Radiative Transfer, 1969 , 9 ( 6 ): 775 − 798 .

PLASS G N . Models for spectral band absorption[J ] . Journal of the Optical Society of America, 1958 , 48 ( 10 ): 690 .

XU H, WANG K . A method for calculating radiant properties of gas by HITRAN data[J ] . Electro-Optic Technology Application, 2018 , 33 ( 02 ): 28 − 31 (in Chinese).

LIU C S, LIU W B. Atmospheric radiation science[M]. Nanjing: Nanjing University Press, 1990 (in Chinese).

TAN H P, XIA X L, LIU L H, et al. Numerical calculation of infrared radiation characteristics and transmission: Computational thermal radiation[M]. Harbin: Harbin Institute of Technology Press, 2006 (in Chinese).

BIAN B H. Analysis and calculation of radiative heat transfer [M]. Beijing: Tsinghua University Press, 1988 (in Chinese).

SHAH N G. A new method of computation of radiant heat transfer in combustion chambers[D]. London: University of London, 1979.

CHANDRASEKHAR S. Radiative transfer[M]. New York: Dover Publications, 1960.

HOWELL J R, PERLMUTTER M . Monte Carlo solution of thermal transfer through radiant media between gray walls[J ] . Journal of Heat Transfer, 1964 , 86 ( 1 ): 116 − 122 .

RAITHBY G D, CHUI E H . A finite-volume method for predicting a radiant heat transfer in enclosures with participating media[J ] . ASME Journal of Heat Transfer, 1990 , 112 : 415 − 423 .

CHUI E H, RAITHBY G D . Implicit solution scheme to improve convergence rate in radiative transfer problems[J ] . Numerical Heat Transfer, Part B: Fundamentals, 1992 , 22 ( 3 ): 251 − 272 .

SELJAK U, ZALDARRIAGA M . A line of sight integration approach to cosmic microwave background anisotropies[J ] . The Astrophysical Journal, 1996 , 469 : 437 − 444 .

LEMAL A, JACOBS C, PERRIN M Y, et al. Simulation of shock tube radiation measurements with a collisional-radiative model[C]// 43rd AIAA Thermophysics Conference, New Orleans, Louisiana. Reston, Virginia: AIAA, 2012: AIAA2012-2868.

LEVIN D A, COLLINS R J, CANDLER G V, et al . Examination of OH ultraviolet radiation from shock-heated air[J ] . Journal of Thermophysics and Heat Transfer, 1996 , 10 ( 2 ): 200 − 208 .

BRANDIS A M, JOHNSTON C O, CRUDEN B A. Non-equilibrium radiation for earth entry[C]// 46th AIAA Thermophysics Conference, Washington, D. C. Reston, Virginia: AIAA, 2016: AIAA2016-3690.

SURZHIKOV S, KOZLOV P. Nonequilibrium radiation NO in shocked air[C]// 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas. Reston, Virginia: AIAA, 2017.

NIU Q L. Phenomenology study on high-speed target radiation in continuous-flow regime[D]. Harbin: Harbin Institute of Technology, 2019.

LAUX C O, SPENCE T G, KRUGER C H, et al . Optical diagnostics of atmospheric pressure air plasmas[J ] . Plasma Sources Science and Technology, 2003 , 12 ( 2 ): 125 − 138 .

GORELOV V A, GLADYSHEV M K, KIREEV A Y, et al . Experimental and numerical study of nonequilibrium ultraviolet NO and N emission in shock layer[J ] . Journal of Thermophysics and Heat Transfer, 1998 , 12 ( 2 ): 172 − 179 .

WU J, YU X L, DUAN R, et al . Influence of excitation and transition rates on ultraviolet radiation of thermal nonequilibrium nitrogen[J ] . Journal of Beijing University of Aeronautics and Astronautics, 2019 , 45 ( 3 ): 472 − 477 (in Chinese).

BOYD I D, PHILLIPS W D, LEVIN D A . Prediction of ultraviolet radiation in nonequilibrium hypersonic bow-shock waves[J ] . Journal of Thermophysics and Heat Transfer, 1998 , 12 ( 1 ): 38 − 44 .

SOHN I, LI Z, LEVIN D A . Effect of nonlocal vacuum ultraviolet radiation on a hypersonic nonequilibrium flow[J ] . Journal of Thermophysics and Heat Transfer, 2012 , 26 ( 3 ): 393 − 406 .

LI Z, SOHN I, LEVIN D A . Modeling of nitrogen monoxide formation and radiation in nonequilibrium hypersonic flows[J ] . Journal of Thermophysics and Heat Transfer, 2014 , 28 ( 3 ): 365 − 380 .

FENG C C. Modeling study on ultraviolet radiation characteristics of bow shock[D]. Harbin: Harbin Institute of Technology, 2015 (in Chinese).

KARPUZCU I T, JOUFFRAY M P, LEVIN D A . Collisional radiative modeling of electronically excited states in a hypersonic flow[J ] . Journal of Thermophysics and Heat Transfer, 2022 , 36 ( 4 ): 982 − 1002 .

KARPUZCU I T, JOUFFRAY M P, LEVIN D A . Effect of oxygen dissociation on nitric oxide ultraviolet emissions[J ] . Journal of Thermophysics and Heat Transfer, 2023 , 37 ( 1 ): 147 − 160 .

KOSSI K K, BOYD I D . Detailed computation of ultraviolet spectra in rarefied hypersonic flow[J ] . Journal of Spacecraft and Rockets, 1998 , 35 ( 5 ): 653 − 659 .

LEVIN D, LAUX C, KRUGER C. A general model for the spectral calculation of OH radiation in the ultraviolet[C]// 26th Plasmadynamics and Lasers Conference, San Diego, CA, USA. Reston, Virginia: AIAA, 1995.

ZHANG L L. Ultraviolet radiation characteristics of typical molecules in plume[D]. Xi′an: Xidian University, 2018 (in Chinese).

ZHENG H J, BAI T Z . Analyzing the ultraviolet radiation of hydroxyl radical chemiluminescence in a motor plume using improved local equilibrium method coupled with Monte Carlo method[J ] . Optik, 2018 , 165 : 159 − 167 .

BAI L, ZHANG D M, LV Q, et al . An improved collision - radiation model of the OH spectrum in the ultraviolet band[J ] . Journal of Quantitative Spectroscopy and Radiative Transfer, 2021 , 271 : 107671 .

SUN M J, BAI L, ZHANG D M, et al . Using a collision-radiation model with extended excitation rates to calculate the OH spectrum in the ultraviolet band[J ] . Optik, 2022 , 268 : 169819 .

LYU J M, HAO J K, CHENG X L, et al . Computational methods of gas radiative noise for hypersonic vehicles[J ] . High Power Laser and Particle Beams, 2016 , 28 ( 08 ): 98 − 105 (in Chinese).

NIU Q L, HE Z H, DONG S K . Prediction of shock-layer ultraviolet radiation for hypersonic vehicles in near space[J ] . Chinese Journal of Aeronautics, 2016 , 29 ( 5 ): 1367 − 1377 .

MU L, MA Y, HE Z H, et al . Radiation characteristics simulati on of non-equilibrium flow field around the hypersonic blunted cone[J ] . Journal of Engineering Thermophysics, 2012 , 33 ( 11 ): 1958 − 1962 (in Chinese).

WANG J. Study on ultraviolet radiation characteristics of rarefied flow field of hypersonic vehicle based on DSMC method[D]. Xi′an: Xidian University, 2022 (in Chinese).

ZHANG T J. Study on the characteristics of thermochemical non-equilibrium flow field and ultraviolet spectrum radiation of hypersonic vehicle tail flame[D]. Xi′an: Xidian University, 2022 (in Chinese).

LI J Y. UV radiation characteristics of hypersonic aircraft plume using spherical harmonics discrete ordinate method[D]. Xi′an: Xidian University, 2018 (in Chinese).

ZHAO T T. Study on ultraviolet radiation transmission characteristics of aircraft plume based on Monte Carlo method[D]. Xi′an: Xidian University, 2018 (in Chinese).

ZHANG D M, BAI L, LYU Q, et al. Image simulation and feature extraction of UV high resolution radiation of plume[J]. Infrared and Laser Engineering, 2021, 50(10): 3788/IRLA20200466 (in Chinese).

NEELE F P, SCHLEIJPEN R M A. Electro-optical missile plume detection[C]//AeroSense 2003. Proc SPIE 5075, Targets and Backgrounds Ⅸ: Characterization and Representation, Orlando, Florida, USA. 2003, 5075: 270-280.

PLASTININ Y, KARABDZHAK G, KHMELININ B, et al. Ultraviolet, visible and infrared spectra modeling for solid and liquid-fuel rocket exhausts[C]//39th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virginia: AIAA, 2001.

GORSHKOV A B . The simulation of ultraviolet radiation under conditions of re-entry of space vehicle from near-earth orbit[J ] . High Temperature, 2010 , 48 ( 1 ): 12 − 22 .

DAI W C. Simulation method of aircraft tail flame image based on ray tracing[D]. Harbin: Harbin Institute of Technology, 2020 (in Chinese).

QI J K, DONG S K . Research on radiation characteristics of typical hypersonic targets[J ] . Tactical Missile Technology, 2021 ( 5 ): 17 − 28 (in Chinese).

EROFEEV A I. Comparison of Monte-Carlo modeling and experimental results of UV-emission from engine exhaust plume interacting with upper atmosphere[C]// The AIP Conference Proceedings, Sydney (Australia). AIP, 2001.

YAN L. Study on related physical mechanism in ultraviolet radiation of missile tail flame[D]. Beijing: Beijing University of Posts and Telecommunications, 2013 (in Chinese).

SHANG J S, ANDRIENKO D A, HUANG P G, et al . A computational approach for hypersonic nonequilibrium radiation utilizing space partition algorithm and Gauss quadrature[J ] . Journal of Computational Physics, 2014 , 266 : 1 − 21 .

CUI J T, ZHANG J Q, DONG C Q, et al . An ultrafast and high accuracy calculation method for gas radiation characteristics using artificial neural network[J ] . Infrared Physics and Technology, 2020 , 108 : 103347 .

GROSS R W F, COHEN N . Temperature dependence of chemiluminescent reactions. Ⅱ. nitric oxide afterglow[J ] . The Journal of Chemical Physics, 1968 , 48 ( 6 ): 2582 − 2588 .

HALL J, PETERSEN E. Kinetics of OH chemiluminescence in the presence of hydrocarbons[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida. Reston, Virginia: AIAA, 2004.

CRUDEN B A, BRANDIS A M. Measurement of radiative non-equilibrium for air shocks between 7-9 km/s [C]//47th AIAA Thermophysics Conference, Denver, Colorado. Reston, Virginia: AIAA, 2017: AIAA2017-4535.

MA P, SHI A H, YANG Y J, et al . Measurement of ray radiation and electromagnetic scattering from hypersonic sphere models and their flow fields in ballistic range[J ] . Acta Armamentarii, 2017 , 38 ( 6 ): 1223 − 1230 (in Chinese).

BRANDIS A M, CRUDEN B A. Benchmark shock tube experiments of radiative heating relevant to earth re-entry[C]//55th AIAA Aerospace Sciences Meeting, Grapevine, Texas. Reston, Virginia: AIAA, 2017.

BRANDIS A M, CRUDEN B A. Shock tube radiation measurements in nitrogen[C]//2018 Joint Thermophysics and Heat Transfer Conference, Atlanta, Georgia. Reston, Virginia: AIAA, 2018. doi:

SMATHERS H, HORAN D, CARDON J, et al. UVPI imaging from the LACE satellite: Starbird rocket plume[J]. NRL Report, 1993, 9546.

REYNOLDS L H, RAMSEY W D, WOLPERT H D, et al. Design and description of the ultraviolet plume instrument (UVPI)[C]//33rd Annual Technical Symposium. Proc SPIE 1158, Ultraviolet Technology Ⅲ, San Diego, USA. 1989, 1158: 196−211.

HARDY J W. Adaptive optics: A progress review[C]//San Diego, '91. Proc SPIE 1542, Active and Adaptive Optical Systems, San Diego, CA, USA. 1991, 1542: 2−17.

WOLFRAM K D, DYMOND K F, BUDZIEN S A, et al. Ionospheric Spectroscopy and Atmospheric Chemistry (ISAAC) experiment on the Advanced Research and Global Observation Satellite (ARGOS): Quick look results[C]//SPIE’s International Symposium on Optical Science, Engineering, and Instrumentation. Proc SPIE 3818, Ultraviolet Atmospheric and Space Remote Sensing: Methods and Instrumentation II, Denver, CO, USA. 1999, 3818: 149−159.

RAULT D F, LOUGHMAN R, SIORIS C. Retrieval of atmospheric ozone and nitrogen dioxide vertical distribution from SAGE Ⅲ limb scattering measurements[C]//Proc SPIE 5235, Remote Sensing of Clouds and the Atmosphere Ⅷ, 2004, 5235: 298-309.

BOVENSMANN H, BURROWS J P, BUCHWITZ M, et al . SCIAMACHY: Mission objectives and measurement modes[J ] . Journal of the Atmospheric Sciences, 1999 , 56 ( 2 ): 127 − 150 .

AMEKUDZI L K, BRACHER A, MEYER J, et al . Lunar occultation with SCIAMACHY: First retrieval results[J ] . Advances in Space Research, 2005 , 36 ( 5 ): 906 − 914 .

FUSSEN D, BAKER N, DEBOSSCHER J, et al . The ALTIUS atmospheric limb sounder[J ] . Journal of Quantitative Spectroscopy and Radiative Transfer, 2019 , 238 : 106542 .

魏京华 . 我国首个空间实验室天宫二号发射成功[J ] . 中国航天, 2016 ( 10 ): 9 .

LEVIN D A, CANDLER G V, COLLINS R J, et al . Examination of theory for bow shock ultraviolet rocket experiments. I[J ] . Journal of Thermophysics and Heat Transfer, 1994 , 8 ( 3 ): 447 − 452 .

LEVIN D A, BRAUNSTEIN M, CANDLER G V, et al . Examination of theory for bow shock ultraviolet rocket experiments. Ⅱ[J ] . Journal of Thermophysics and Heat Transfer, 1994 , 8 ( 3 ): 453 − 459 .

KARABADZHAK G, PLASTININ Y, AFANASIEV A, et al. Measurements of the progress-M main engine retrofiring plume at orbital conditions[C]//37th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virginia: AIAA, 1999.

GIMELSHEIN S F, LEVIN D A, DRAKES J A, et al . Ultraviolet radiation modeling from high-altitude plumes and comparison with Mir data[J ] . AIAA Journal, 2000 , 38 : 2344 − 2352 .

WINTER M, HERDRICH G. Spectroscopic observation of the STARDUST re-entry in the near UV[C]//39th AIAA Thermophysics Conference, Miami, Florida. Reston, Virginia: AIAA, 2007.

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Dynamic ablation morphology measurement of thermal protection materials using structured light vision

Installation effects on propeller tone noise

Research on the characteristics of water droplets impacting moving superhydrophobic surfaces and its regulation

Research progress on noise reduction of centrifugal fans

Analysis of damping and cross dynamic derivative characteristics for a quasi-HyTRV lifting body

Related Author

No data

Related Institution

No data

AI问答

⁰