| Citation: | LIU Yongping, ZHA Jun, HU Zhe, et al. Correlation correction of aerodynamic characteristics in heavy gas medium[J]. Journal of Aerospace Power, 2025, 40(10):20230748 doi: 10.13224/j.cnki.jasp.20230748 |
The steady transonic aerodynamic characteristics of supercritical airfoil RAE2822 and CHN-T2 in heavy gas and air were calculated by CFD. Based on the transonic similarity law and critical specific heat ratio, aerodynamic data in heavy gas medium were converted to data in equivalent air medium. The results showed that the surface pressure distributions in these two media were in good agreement with each other. For flutter tests, the slope of the lift coefficient curve and pitch moment coefficient curve at small angles of attack raised concern, after similarity correction, the slope values obtained in heavy gas medium was less than 2% different from that in air medium, which met the requirements of flutter test.
| [1] |
GARRICK I E, REED W H. Historical development of aircraft flutter[J]. Journal of Aircraft, 1981, 18(11): 897-912. doi: 10.2514/3.57579
|
| [2] |
GARRETSON D, MAIR H, MARTIN C, et al. Review of CFD capabilities[R]. Washington, US: Institute for Defense Analysis, Science and Technology Policy Institute, 2005.
|
| [3] |
COLE S, GARCIA J. Past, present, and future capabilities of the Transonic Dynamics Tunnel from an aeroelasticity perspective[R]. AIAA-2000-1767, 2000.
|
| [4] |
王赫喆. 跨声速颤振模型超重问题研究[J]. 飞机设计, 2014, 34(4): 10-12. WANG Hezhe. Study on the problem of overweight flutter model on the transonic wind-tunnel test[J]. Aircraft Design, 2014, 34(4): 10-12. (in Chinese
WANG Hezhe. Study on the problem of overweight flutter model on the transonic wind-tunnel test[J]. Aircraft Design, 2014, 34(4): 10-12. (in Chinese)
|
| [5] |
COLE S R, NOLL T E, PERRY B. Transonic dynamics tunnel aeroelastic testing in support of aircraft development[J]. Journal of Aircraft, 2003, 40(5): 820-831. doi: 10.2514/2.6873
|
| [6] |
COLE S R, RIVERA J A J. The new heavy gas testing capability in the NASA Langley transonic dynamics tunnel[R]. NASA-TM-112702, 1997.
|
| [7] |
IVANCO T G. Unique testing capabilities of the NASA langley transonic dynamics tunnel, an exercise in aeroelastic scaling[R]. AIAA-2013-2625, 2013.
|
| [8] |
PERR B, NOLL T, SCOTT R. Contributions of the transonic dynamics tunnel to the testing of active control of aeroelastic response[R]. AIAA-2000-1769, 2000.
|
| [9] |
COLE S, KELLER D, PIATAK D. Contributions of the NASA Langley transonic dynamics tunnel to launch vehicle and spacecraft development[R]. AIAA-2000-1772, 2000.
|
| [10] |
WILLIAM YEAGER J Jr, KVATERNIK R. Contributions of the Langley transonic dynamics tunnel to rotorcraft technology and development[R]. AIAA-2000-1771, 2000.
|
| [11] |
YEAGER W T J, KVATERNIK R G. A historical overview of aeroelasticity branch and transonic dynamics tunnel contributions to rotorcraft technology and development[R]. NASA/TM-2001-211054, 2001.
|
| [12] |
张汇卓. 重气体环境机翼气动特性数值模拟研究[D]. 北京: 军事科学院, 2021. ZHANG Huizhuo. Numerical simulation study on aerodynamic characterristics of wing in heavy gas environment[D]. Beijing: Academy of Military Science, 2021. (in Chinese
ZHANG Huizhuo. Numerical simulation study on aerodynamic characterristics of wing in heavy gas environment[D]. Beijing: Academy of Military Science, 2021. (in Chinese)
|
| [13] |
查俊, 曾开春, 寇西平, 等. 重气体介质中超临界翼型跨声速流动特性[J]. 航空动力学报, 2021, 36(9): 1894-1905. ZHA Jun, ZENG Kaichun, KOU Xiping, et al. Transonic flow characteristics of supercritical airfoil in heavy gas medium[J]. Journal of Aerospace Power, 2021, 36(9): 1894-1905. (in Chinese
ZHA Jun, ZENG Kaichun, KOU Xiping, et al. Transonic flow characteristics of supercritical airfoil in heavy gas medium[J]. Journal of Aerospace Power, 2021, 36(9): 1894-1905. (in Chinese)
|
| [14] |
刘永平, 寇西平, 查俊, 等. 重气体介质的等熵流动特性[J]. 航空动力学报, 2025, 40(9): 20230421. LIU Yongping, KOU Xiping, ZHA Jun, et al. Isentropic flow characteristics of heavy gas medium[J]. Journal of Aerospace Power, 2025, 40(9): 20230421. (in Chinese
LIU Yongping, KOU Xiping, ZHA Jun, et al. Isentropic flow characteristics of heavy gas medium[J]. Journal of Aerospace Power, 2025, 40(9): 20230421. (in Chinese)
|
| [15] |
HUBER P W. Use of Freon-12 as a fluid for aerodynamic testing[R]. NACA-TN-1024, 1946.
|
| [16] |
SCHWARTZBERG M A. A study of the use of Freon-12 as a wind-tunnel testing medium at low supersonic Mach numbers[R]. NACA-RM-L52J07, 1952.
|
| [17] |
VON DOENHOFF A E, BRASLOW A L, SCHWARTZBERG M A. Studies of the use of Freon-12 as a wind tunnel testing medium[R]. NACA-TN-3000, 1953.
|
| [18] |
POZNIAK O M. Investigation into the use of Freon 12 as a working medium in a high-speed wind tunnel[D]. Cranfield, UK: Cranfield University, 1957.
|
| [19] |
ANDERSON W. A numerical study on the use of sulfur hexafluoride as a test gas for wind tunnels[R]. AIAA-1990-1421, 1990.
|
| [20] |
BONHAUS D L, ANDERSON W K. Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils[R]. NASA TP-3496, 1995.
|
| [21] |
ANDERS J, ANDERSON W, MURTHY A. The use of heavy gas for increased Reynolds numbers in transonic wind tunnels[R]. AIAA-1998-2882, 1998.
|
| [22] |
CAHILL J F, CONNOR P C. Correlation of data related to shock-induced trailing-edge separation and extrapolation to flight Reynolds number[R]. NASA CR-3178, 1979.
|
| [23] |
BENDIKSEN O. Role of shock dynamics in transonic flutter[R]. AIAA-1992-2121, 1992.
|
| [24] |
BENDIKSEN O. Influence of shocks on transonic flutter of flexible wings[R]. AIAA-2009-2313, 2009.
|
| [25] |
VON KARMAN T. The similarity law of transonic flow[J]. Journal of Mathematics and Physics, 1947, 26(1/2/3/4): 182-190.
|
| [26] |
GUDERLEY G, YOSHIHARA H. The flow over a wedge profile at Mach number 1[J]. Journal of the Aeronautical Sciences, 1950, 17(11): 723-735. doi: 10.2514/8.1782
|
| [27] |
SPREITER J R. On the application of transonic similarity rules to wings of finite span[R]. NACA Report1153, 1953.
|
| [28] |
SPREITER J R. On alternative forms for the basic equations of transonic flow theory[J]. Journal of the Aeronautical Sciences, 1954, 21(1): 70-72. doi: 10.2514/8.2926
|
| [29] |
刘沛清. 空气动力学[M]. 北京: 科学出版社, 2021.
|
| [30] |
THOMPSON P A. A fundamental derivative in gasdynamics[J]. The Physics of Fluids, 1971, 14(9): 1843-1849. doi: 10.1063/1.1693693
|
| [31] |
BELL I H, WRONSKI J, QUOILIN S, et al. Pure and pseudo-pure fluid thermophysical property evaluation and the open-source thermophysical property library CoolProp[J]. Industrial & Engineering Chemistry Research, 2014, 53(6): 2498-2508.
|