Search alternatives:
"shock wave" » "stock wave" (Expand Search), "shock have" (Expand Search)
Showing 1 - 20 results of 45 for search '"shock wave"', query time: 0.13s Refine Results
  1. 1
  2. 2
    Published 1987
    Subjects: “…Shock waves Measurement Congresses.…”
  3. 3
    “… sensors, which allow the shock wave strength, shock wave speed and peak pressure to be analysed…”
    Get full text
    Get full text
  4. 4
    Published 1997
    Subjects: “…Shock waves…”
  5. 5
  6. 6
    “… pressure and shock wave speed change of Air-Air as a driver/driven gas are then presented and compared…”
    Get full text
    Get full text
    Get full text
  7. 7
    by Crasta, Asha, Khan, Sher Afghan
    Published 2016
    “… at the leading edge of the wing. Whereas, in the case of detached shock wave, this theory is not valid.…”
    Get full text
    Get full text
    Get full text
  8. 8
    by Norul Husna, Ibrahim
    Published 2012
    “… of shock wave.It's also able to measure aerodynamic quantities such as pressure,skin friction,lift,drag…”
    Get full text
    Get full text
    Get full text
  9. 9
    by Crasta, Asha, Khan, Sher Afghan
    Published 2014
    “… theory. The Present theory is valid only when the shock wave is attached with the leading edge…”
    Get full text
    Get full text
    Get full text
  10. 10
    “…-kinetic scheme. A typical two-dimensional regular reflection of an oblique shock wave from a solid surface…”
    Get full text
    Get full text
  11. 11
    by Crasta, Asha, Khan, Sher Afghan
    Published 2014
    “… in pitch. The present theory is valid only when the shock wave is attached with the nose of the wedge. From…”
    Get full text
    Get full text
    Get full text
    Get full text
  12. 12
    by Crasta, Asha, Khan, Sher Afghan
    Published 2015
    “…. The Present theory is valid only when the shock wave is attached with the wing leading edge, for detached…”
    Get full text
    Get full text
    Get full text
  13. 13
    by Crasta, Asha, Khan, Sher Afghan
    Published 2013
    “… the shock wave is attached to the leading edge of the wing. The expressions derived for stability…”
    Get full text
    Get full text
    Get full text
  14. 14
    “… angle theta and low Mach number shock wave will be detached. The surface pressure derivative with Mach…”
    Get full text
    Get full text
    Get full text
    Get full text
  15. 15
  16. 16
  17. 17
    by Crasta, Asha, Khan, Sher Afghan
    Published 2014
    “… in pitch. The present theory is valid only when the shock wave is attached with the nose of the wedge…”
    Get full text
    Get full text
    Get full text
    Get full text
  18. 18
  19. 19
    “… derivatives in pitch has been obtained. The present theory is valid only for shock wave which is attached…”
    Get full text
    Get full text
    Get full text
    Get full text
  20. 20
Search Tools: RSS Feed Email Search