导航

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1985, Vol. 6 ›› Issue (4): 393-396.

• 论文 • Previous Articles     Next Articles

CALCULATION OF SUPERSONIC FLOWS AROUND A THREE-DIMENSIONAL WING AND A WAISTED BODY WITH CHARA- CTERISTIC METHOD IN STREAM SURFACE COORDINATES

Wang Baoyu   

  1. Beijing Institute of Aeronautics and Astronautics
  • Received:1984-06-25 Revised:1900-01-01 Online:1985-08-25 Published:1985-08-25

Abstract: According to the exact characteristic surface equation of three dimensions and the physical relations along bicharacteristics in stream surface coordinates of Ref. 1 , the pressure distributions of circula-elliptic delta wing and waisted body are calculated with "real" characteristic method. The results are compared with those of Refereces 2,3,4 and 6.