| Citation: | Effect of movable flat baffles plenum volume on pressure distortion flow field of engine[J]. Journal of Aerospace Power, 2018, 33(9): 2242-2247. doi: 10.13224/j.cnki.jasp.2018.09.022
|
| [1] |
刘大响,叶培梁,胡骏,等.航空燃气涡轮发动机稳定性设计与评定技术［M］.北京:航空工业出版社,2004.
|
| [2] |
国防科学技术工业委员会.航空燃气涡轮发动机稳定性设计与评定方法:GJB/Z224-2005［S］.北京:中国航空工业第一集团公司,2005：15-20.
|
| [3] |
田金虎,乔渭阳,彭生红.航空发动机高空压力畸变试验［J］.航空动力学报,2014,29(4):817-823.TIAN Jinhu,QIAO Weiyang,PENG Shenghong.The experimental investigation on aero-engine altitude simulated inlet total pressure distortion［J］.Journal of Aerospace Power,2014,29(4):817-823.(in Chinese)
|
| [4] |
BEALE D K,CRAMER K B.Development of improved method for simulation aircraft inlet distortion in turbine engine ground tests［R］.AIAA-2002-3045,2002.
|
| [5] |
BION J R.Steady and unsteady distorted inlet flow simulation for engine ground tests［R］.AIAA 84-1490,1984.
|
| [6] |
江勇,张发启.基于实验的插板式进气畸变稳态压力场估计［J］.空军工程大学学报(自然科学版),2007,8(2):1-3.JIANG Yong,ZHANG Faqi.Base on experiment the air inlet flow steady pressure distortion field estimate with the inserted board［J］.Journal of Air Force Engineering University (Natural Science Edition),2007,8(2):1-3. (in Chinese)
|
| [7] |
顾卫群,秦敏,陈建民,等.可移动插板式压力畸变发生器的设计与试验［C］∥中国燃气涡轮研究院40周年院庆文集.四川 绵阳:中国燃气涡轮研究院,2005:26-31.
|
| [8] |
李名魁,张发启,王如根.插板式畸变发生器出口动态压力信号的功率谱分析［J］.燃气涡轮试验与研究,2002,15(4):17-20.LI Mingkui,ZHANG Faqi,WANG Rugen.Power spectrum analysis of dynamic pressure signal by inlet flat baffle［J］.Gas Turbine Experiment and Research,2002,15(4):17-20.(in Chinese)
|
| [9] |
PETER G,MARTIN H.Modeling the dynamics of supersonic inlet/gas-turbine engine system for large-amplitude high-frequency disturbances［R］.AIAA-2000-3594,2000.
|
| [10] |
OVERALL B W.Evaluation of an airjet distortion generator used to produce steady-state total-pressure distortion at the inlet of turbine engines［R］.AEDC-TR-76-141,1976.
|
| [11] |
BRIMELOW B,COLLINS T P,PFEFFERKORN G A.Engine testing in a dynamic environment［R］.AIAA 74-1198,1976.
|
| [12] |
LAZALIER G R,TATE J T.Development of a prototype discrete frequency total-pressure fluctuation generator for jet engine/inlet compatibility investigation［R］.Air Force Airframe Propulsion Compatibility Symposium,AFAPL-TR-69-103,1970.
|
| [13] |
REYNOLDS G.An experimental evaluation of unsteady flow effects on an axial compressor-p3 generator program［R］.Air Force Airframe Propulsion Compatibility Symposium,AFAPL-TR-73-43,1973.
|
| [14] |
程邦勤,陶增元,李军.某型涡扇发动机进气总压畸变的试验研究［J］.推进技术,2003,24(1):21-23.CHENG Bangqin,TAO Zengyuan,LI Jun.Aerodynamic stability analysis of inlet total pressure distortion for turbofan［J］.Journal of Propulsion Technology,2003,24(1):21-23.(in Chinese)
|
| [15] |
李文峰,马利东.某涡扇发动机压力畸变评定技术［J］.西北工业大学学报,2003,21(5):540-543.LI Wenfeng,MA Lidong.Method and experimental facility for assessing pressure distortion of a certain turbofan engine［J］.Journal of Northwestern Polytechnical University,2003,21(5):540-543.(in Chinese)
|
| [16] |
SMITH R E.Marrying airframes and engines in ground test facilities:an evolutionary revolution［R］.AIAA 95-0950,1995.
|
| [17] |
OGORODNIKOV D A.Real-time simulation of maneuverable aircraft flight conditions on altitude test cell［R］.AIAA 93-1845,1993.
|
| [18] |
DAVIS M,BEALE D,BOYER K,et al.An example for integrated gas turbine engine testing and analysis using modeling and simulation［R］:Las Cruces,NM，US:ITEA Modeling and Simulation Conference,2006.
|
| [19] |
CHUNG K,HOSNY W M,STEENKEN W G.Aerodynamic stability analysis of NASA J85-13 planar pressure pulse generator installation［R］.NASA-CR-165141,1980.
|
DownLoad: