导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (6): 11-15.

• 论文 • Previous Articles     Next Articles

TRANSONIC AERODYNAMIC DESIGN OF DELTA WINGS UNDERGOING BODY EFFECTS

Lai Yuanchao   

  1. Chengdu Aircraft Design and Research Institute, Chengdu, 610041
  • Received:1995-06-20 Revised:1995-12-05 Online:1996-12-25 Published:1996-12-25

Abstract: An inverse aerodynamic wing design method by residual correction for prescribed pressure is extended to the aerodynamic design of delta wings undergoing body effects in transonic flow. The resolution of some difficulties about these design procedure is given by a body delta wing combination design example.

Key words: delta wings, aerodynamic configuration, transonic flow, design analysis

CLC Number: