[1] MANNÉE J. Wind tunnel investigation of the influence of the aircraft configuration on the yawing-and rolling moments of a twin-engined propeller driven aircraft with one engine inoperative:NLL A-1508 B[R]. 1962. [2] SCHROIJEN M J T, VELDHUIS L L M, SLINGERLAND R. Propeller slipstream investigation using the Fokker F27 wind tunnel model with flaps deflected[C]//ICAS2008, 2008. [3] KROO I. Propeller/wing integration for minimum induced loss[J]. Journal of Aircraft, 1986, 23(7):561-565. [4] VAN NISPEN A. Slipstream effects on the static lateral and directional control of a multi-engined propeller aircraft with one engine inoperative[D]. Delft:Delft University of Technology, 2002. [5] RAUHUT P. Modelling of the slipstream effects on the static lateral and directional stability and control of a single engine propeller aircraft[D]. Delft:Delft University of Technology, 2002. [6] RENOOIJ M. Propeller slipstream effects and wing-fuselage lift carry-over effects on the stability of a single engine propeller airplane[D]. Delft:Delft University of Technology, 2005. [7] VELDHUIS L L M. Propeller wing aerodynamic interference[D]. Delft:Delft University of Technology, 2005. [8] SCHROIJEN M J T. Propeller installation effects on lateral stability and control of multi-engine propeller aircraft[D]. Delft:Delft University of Technology, 2006. [9] SCHROIJEN M J T, SLINGERLAND R. Propeller slipstream effects on directional aircraft control with one engine inoperative:AIAA-2007-1046[R]. Reston, VA:AIAA, 2007. [10] MUKUND R,CHANDAN K A. Velocity field measurements in the wake of a propeller model[J]. Experiment in Fluids, 2016, 57:154. [11] Jr COE P L, GENTRY C L, DUNHAM D M. Low speed wind-tunnel tests of an advanced eight-bladed propeller:NASA TM 86364[R]. Washington, D.C.:NASA, 1985. [12] VAN DEN BORNE P C M, VAN HENGST J. Investigation of propeller slipstream effects on the Fokker 50 through in-flight pressure measurements:AIAA-1990-3064[R]. Reston, VA:AIAA, 1990. [13] OHMAN L H, NGUYEN V D, BARBER D J. Probe interference on flow measurements in propeller near slipstream[J]. Journal of Aircraft, 1995, 32(4):887-888. [14] DETERS R W. Performance and slipstream characteristics of small-scale propellers at low Reynolds numbers[D]. Illinois:University of Illinois, 2014. [15] DETERS R W. Slipstream measurements of small propellers at low Reynolds numbers:AIAA-2015-2265[R]. Reston, VA:AIAA, 2015. [16] 李征初, 王勋年, 陈洪, 等. 螺旋桨滑流对飞机机翼流场影响试验研究[J]. 流体力学实验与测量,2000, 14(2):44-48. LI Z C, WANG X N, CHEN H, et al. Experimental Research of influenceof propeller slipstream on wing flow field[J]. Experiments and Measurements in Fluid Mechanics, 2000, 14(2):44-48(in Chinese). [17] STALLA A, GUJ G, DI FELICE F. Propeller wake flowfield analysis by means of LDV phase sampling techniques[J]. Experiments in Fluids, 2000, 28:1-10. [18] COTRONI A, DI FELICE F, ROMANO G P, et al. Investigation of the near wake of a propeller using particle image velocimetry[J]. Experiments in Fluids, 2000, 29(S1):227-236. [19] LEE S J, PAIK B G, YOON J H, et al. Three-component velocity fluid measurements of propeller wake using a stereoscopic PIV technique[J]. Experiments in Fluids, 2004, 36:575-585. [20] FELLI M, DI FELICE F, GUJ G, et al. Analusis of the propeller wake evolution by pressure and velocity phase measurements[J]. Experiments in Fluids, 2006, 41:441-451. [21] FELLI M, GUJ G, CAMUSSI R. Effect of the number of blades on propeller wake evolution[J]. Experiments in Fluids, 2008, 44:409-418. [22] SHKARAYEV S, KURNOSOV V, GOMEZ D. Flow studies around a small propeller in coverting maneuver:AIAA-2017-3742[R]. Reston, VA:AIAA, 2017. [23] LI Q X, ÖZTÜRK K, SINNIGE T. Design and experimental validation of swirl recovery vanes for propeller propusion systems:AIAA-2017-3571[R]. Reston, VA:AIAA, 2017. [24] ROOSENBOOM E W M, STÜRMER A, SCHRÜDER A. Advanced experimental and numerical validation and analysis of propeller slipstream flows[J]. Journal of Aircraft, 2010, 47(1):284-291. |