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COMPUTATION OF A CONTROLLED STORE SEPARATION FROM A CAVITY

机译:COMPUTATION OF A CONTROLLED STORE SEPARATION FROM A CAVITY

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摘要

Coupling of the Reynolds-averaged Navier-Stokes equations, rigid-body dynamics, and a pitch-attitude control law is demonstrated in two and three dimensions, The application problem was the separation of a canard-controlled store from an open-flow rectangular cavity at a freestream Mach number of 1.2. The transient flowfield was computed using a diagonal scheme in an overset mesh framework, with the resultant aerodynamic loads used as the forcing functions in the nonlinear dynamics equations. The proportional and rate gyro sensitivities were computed via pole placement techniques for the linearized dynamical equations, in which computed aerodynamic stability derivatives were used, In two dimensions, a comparison between full and linearized now equations for a perturbed pinned missile was made, and a controlled store was found to possess improved separation characteristics over a canard-fixed store, in three dimensions, trajectory comparisons with quasisteady wind-tunnel data for the canard-fixed case were made, Comparisons of canard-fixed and canard-active simulations showed that controlled store offers only modest improvements in cavity separation characteristics for these high-ejection rate cases.

著录项

  • 来源
    《Journal of aircraft》 |1995年第4期|846-852|共7页
  • 作者

    Atwood CA.;

  • 作者单位

    NASA AMES RES CTR MOFFETT FIELD CA 94035 USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 英语
  • 中图分类 航空;
  • 关键词

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