某降落伞风洞试验支撑装置力学性能分析
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摘要
以某火星降落伞在2.4 m×2.4 m跨声速风洞的空气动力试验为背景,设计了其风洞试验的结构支撑装置,并对其进行了力学建模,得到了支持装置的数学模型,根据得到的数学模型对重力影响特性、结构静力学特性和动力学特性进行了仿真分析。结果表明设计的某火星降落伞2.4 m跨声速风洞试验支撑装置具有较好的强度特性和刚度特性,满足试验要求。
The 2.4m×2.4m transonic wind tunnel test for a parachute for Mars probe is investigated in this paper. The structural support device for the wind tunneltest is designed and its mechanical model is established. According to the influence of the gained mathematical model on the gravity and the static and dynamic property, the simulation analysis is done. The results indicate that the designed Mars probe parachute has better strength and larger stiffness. This design meets the requirements of the wind tunnel testing.
The 2.4m×2.4m transonic wind tunnel test for a parachute for Mars probe is investigated in this paper. The structural support device for the wind tunneltest is designed and its mechanical model is established. According to the influence of the gained mathematical model on the gravity and the static and dynamic property, the simulation analysis is done. The results indicate that the designed Mars probe parachute has better strength and larger stiffness. This design meets the requirements of the wind tunnel testing.
引文
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[17] Manley C,Butler J.The Design,Testing,Certification and Production of an Emergency Parachute for Use in Light Aircraft [C].San Diego,California,1981.
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[28] Tyagi J K,Kumar P.Parametric Study of Unicross Parachute Under Infinite and Finite Mass Conditions [C].San Diego,CA,1991.
[29] Stein K,Benney R,Tezduyar T,et al.Fluid—Structure Interactions of a Cross Parachute:Numerical Simulation[J].Comput.Methods Appl.Mech.Engrg,2001(191):673-687.
[30] Johari H,Levshin A.Interaction of a Line Vortex with Around Parachute Canopy[J].Journal of Fluids and Structures,2009(25):1258-1271.
[31] Karagiozis K,Kamakoti R,Cirak F,et al.A Computational Study of Supersonic Disk-Gap-Band Parachutes Using Large-Eddy Simulation Coupled to a Structural Membrane[J].Journal of Fluids and Structures,2011(27):175-192.
[32] Kim J,Li Y,Li X.Simulation of Parachute Fsi Using the Front Tracking Method[J].Journal of Fluids and Structures,2013(37):100-119.
[33] Shen G,Xia Y,Sun H.A 6Dof Mathematical Model of Parachute in Mars Edl[J].Advances in Space Research,2015(55):1823-1831.
[34] Gao Z,Charles R D,Li X.Numerical Modeling of Flow through Porous Fabric Surface in Parachute Simulation[J].Aiaa Journal,2017,55(2):686-690.
[2] 江桂清.降落伞风洞试验中的几个主要问题[J].航空学报,1993,14(6):230-235.
[3] Witkowski A,Bruno R.Mars Exploration Rover Parachute Decelerator System Program Overview [C].Monterey,California,2003.
[4] Whitmore S A,Cobleigh B R,Jacobson S R,et al.Development and Testing of a Drogue Parachute System for X-37 Altv / B-52H Separation [C].Reno,Nevada,2004.
[5] Heinrich H G,Noreen R A.Analysis of Parachute Opening Dynamics with Supporting Wind Tunnel Experiments [C].El Centro,California,1968.
[6] Heinrich H G,Hektner T R.Flexibility as Parameter of Model Parachute Performance Characteristics [C].Dayton,Ohio,1970.
[7] Mcvey D F,Pepper W B,Reed J F.A Paarametric Wind Tlxinel Study of Ribbon Parachutes [C].Albuquerque,New Mexico,1975.
[8] Croll R H,Berg D E,Johnson C S,et al.Computerized Video Instrumentation Technique for Wind Tunnel Testing of Parachutes [C].San Diego,California,1981.
[9] Kemnitz J.Low Cost Techniques for Glldlng Parachute Testing [C].San Diego,CA,1991.
[10] Underwood J C,Saunders A,Rogers S B,et al.Subsonic Wind Tunnel Testing of Various Parachute Types [C].Daytona Beach,FL,2015.
[11] O'Farrell C,Brandeau E J,Tanner C L,et al.Reconstructed Parachute System Performance During the Second Ldsd Supersonic Flight Dynamics Test [C] .Daytona Beach,FL,2015.
[12] Steinberg S,Siemers P M,Slayman R G.Development of the Viking Parachute Configuration by Wind-Tunnel Investigation[J].Journal of Aircraft,1974,11(2):101-107.
[13] Rychnovsky R E.A Lifting Parachute for Very Low-Altitude,Very High-Speed Deliveries [C].Albuquerque,New Mexico,1975.
[14] Rychnovsky R E,Everett R N.Wind Tunnel Tests.To Evaluate a Lifting Transonic Parachute [C].ALbuquerque,New Mexico,1975.
[15] Bacchus D L,Vickers J R,Foughner J T.Wind Tunnel Investigation of Space Shuttle Solid Rocket Booster Drogue Paraciiutes and Deployment Concepts [C].Albuquerque,New Mexico,1975.
[16] Pepper W B,Reed J F.Parametric Study of Parachute Pressure Distribution by Wind Tunnel Testing[J].Journal of Aircraft,1976,13(11):895-900.
[17] Manley C,Butler J.The Design,Testing,Certification and Production of an Emergency Parachute for Use in Light Aircraft [C].San Diego,California,1981.
[18] Croll R H,Klima P C,Tate R E,et al.Summary of Parachute Wind Tunnel,Testing Methods at Sandia National Laboratories [C].San Diego,California,1981.
[19] Wolf D F,Croll R H.Wind-Tunnel Measurements of Dynamic Reefing Line Force in Ribbon Parachutes[J].Journal of Aircraft,1981,18(1):30-34.
[20] Wolf D F.A Coupling Apparent Mass for Parachute Inflation Equations [C].Cocoa Beach,FL,1989.
[21] Wolf D.Parachute Opening Shock [C].Toulouse,France,1999.
[22] Taylor A P,Sinclair R J,Allamby R D.Design and Testing of the Kistler Landing System Parachutes [C].Toulouse,France,1999.
[23] Zumwalt C H,Cruz J R,Keller D F,et al.Wind Tunnel Test of Subscale Ringsail and Disk-Gap-Band Parachutes [C].Washington,D.C.,2016.
[24] Jin Z,Pasqualini S,Yang Z.Experimental Investigation of the Flow Structures in the Wake of a Cross Parachute Canopy[J].European Journal of Mechanics,B/Fluids,2016(60):70-81.
[25] Purvis J W.Parachute Drag and Radial Force [C].Reno,Nevada,1986.
[26] Macha J M,Buffington R J.Wall-Intebferwce Corrections for Parachutes in a Closed Wnll Tunnel [C].Cocoa Beach,FL,1989.
[27] Doherr K F,Schilling H.9Dof-Simulation of Rotating Parachute Systems [C].San Diego,CA,1991.
[28] Tyagi J K,Kumar P.Parametric Study of Unicross Parachute Under Infinite and Finite Mass Conditions [C].San Diego,CA,1991.
[29] Stein K,Benney R,Tezduyar T,et al.Fluid—Structure Interactions of a Cross Parachute:Numerical Simulation[J].Comput.Methods Appl.Mech.Engrg,2001(191):673-687.
[30] Johari H,Levshin A.Interaction of a Line Vortex with Around Parachute Canopy[J].Journal of Fluids and Structures,2009(25):1258-1271.
[31] Karagiozis K,Kamakoti R,Cirak F,et al.A Computational Study of Supersonic Disk-Gap-Band Parachutes Using Large-Eddy Simulation Coupled to a Structural Membrane[J].Journal of Fluids and Structures,2011(27):175-192.
[32] Kim J,Li Y,Li X.Simulation of Parachute Fsi Using the Front Tracking Method[J].Journal of Fluids and Structures,2013(37):100-119.
[33] Shen G,Xia Y,Sun H.A 6Dof Mathematical Model of Parachute in Mars Edl[J].Advances in Space Research,2015(55):1823-1831.
[34] Gao Z,Charles R D,Li X.Numerical Modeling of Flow through Porous Fabric Surface in Parachute Simulation[J].Aiaa Journal,2017,55(2):686-690.