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强化团的教育职能

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作者 韩非 王亚奇
出处 《石油政工研究》 2002年第2期46-47,共2页
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  • 1[1]ER-EL J , SEGINER A . Vertex trajectories and break down on wing-canard configurations. Journal of Aircraft,1985,22(8):641~648.
  • 2[2]ER-EL J .Effect of wing/canard interference on the loading of a delta wing. Journal of aircraft, 1988,25(1):18~24.
  • 3[3]OELKER H CHR.,HUMMEL,D . Investigation on the vorticity sheets of a close-coupled delta-canard configuration.Journal of aircraft,1989,26(7):657~666.
  • 4[4]HUMMEL D , OELKER H Chr . Low-speed characteristics for the wing-canard configuration of the international vertex flow experiment.Journal of aircraft,1994,31(4):868~878.
  • 5[5]RICHARD M Howard,JOHN F O'leary . Flow field study of a closed-coupled canard configuration.Journal of aircraft, 1994,31(4):908~914.
  • 6[1]Oelker H Chr, Hummel D. Investigation on the vorticity sheets of a close-coupled delta-canard configuration[J]. J Aircraft,1989, 26(7):657-666
  • 7[2]Hummel D, Oelker H Chr. Low-speed characteristics for the wing-canard configuration of the international vertex flow experiment[J]. J Aircraft,1994, 31(4): 868-878.
  • 8[3]Er-El J, Seginer A. Voertex trajectories and break down on wing-canard configurations[J]. J Aircraft,1985, 22(8):641-648.
  • 9[4]Er-El J. Effect of wing/canard interference on the loading of a delta wing[J]. J Aircraft, 1988, 25(1):18-24
  • 10[5]Howard R M. Kersh,Jr J M. Effect of canard deflection on enhanced lift for a close-coupled-canard configuration[R]. AIAA-3222-CP,1991.

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