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Forecasting Method of Shock-Standoff Distance for Forward-Facing Cavity

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Shock Wave Interactions (RaiNew 2017)

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Abstract

Experiments are performed on a cylinder with a forward-facing cavity at the tip in the flow of \( M_{\infty } = 10 \) in FD-14A shock tunnel. The shock shape, shock-standoff distance, and oscillation characteristics are captured by the high-speed movie, and the dynamic pressure response is used to correlate with the acoustic characteristics of the cavity base through the transducer. By analyzing the amount of experimental and numerical results abroad, a forecasting method for shock-standoff distance is proposed. Combination of organ-pipe theory with experimental results of oscillation frequency validates the applicability and effectiveness of the method. Results of shock-standoff distance and oscillation frequency are also obtained for experiments in FD-14A shock tunnel. The forecasting results of oscillation frequency are in accordance with the experimental results. Furthermore, the oscillation amplitude and average velocity of the shock wave are analyzed for forward-facing nose cavity at \( M_{\infty } = 10 \).

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References

  1. Ladoon, D.W., Schneider, S.P., Schmisseur, J.D.: Physics of resonance in a supersonic forward-facing cavity. J. Spacecr. Rocket. 35(5) (1998)

    Google Scholar 

  2. huebner, L.D., Utreja, L.R., Mach 10 bow-shock behavior of a forward-facing nose cavity. J. Spacecr. Rocket. 30(3), 291–297 (1993)

    Google Scholar 

  3. Engblom, W.A., Goldstein, D.B., Ladoon, D.: Fluid dynamics of hypersonic forward-facing cavity flow. AIAA (1996)

    Google Scholar 

  4. Engblom, W.A., Yuceil, K.B., Goldstein, D.B.: Experimental and numerical study of hypersonic forward-facing cavity flow. J. Spacecr. Rocket. 33(3), 353–359 (1996)

    Article  Google Scholar 

  5. Yadav, R., Guven, U.: Aerothermodynamics of a hypersonic vehicles with a forward facing parabolic cavity at nose. J. Aerosp. Eng. 228(10), 1863–1874 (2014)

    Google Scholar 

  6. Yadav, R., Guven, U.: Aerodynamic heating of a hypersonic projectile with forward-facing ellipsoid cavity at nose. J. Spacecr. Rocket. 52(157--165) (2015)

    Google Scholar 

  7. Hartmann, J., Troll, B.: On a new method for the generation of sound waves. Phys. Rev. 20, 719–727 (1922)

    Article  Google Scholar 

  8. Sambamurthi, J.K., huebner, L.D., Utreja, L.R.: Hypersonic flow over a cone with nose cavity. In: AIAA 19th Fluid Dynamics, Plasma Dynamics and Lasers Conference, Hawaii. (1987)

    Google Scholar 

  9. Marquart, E.J., Grubb, J.P.: Bow shock dynamics of a forward-facing nose cavity. In: AIAA 11th Aerocoustics Conference, Sunnyvale. (1987)

    Google Scholar 

  10. Saravanan, S., Jagadeesh, G., Reddy, K.P.: Investigation of missile-shaped body with forward-facing cavity at Mach 8. J. Spacecr. Rocket. 46(3) (2009)

    Google Scholar 

  11. Engblom, W.A., Goldstein, D.: Acoustic Analogy for Oscillations Induced by Supersonic Flow over a Forward-Facing Nose Cavity. In: 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, Florida. (2009)

    Google Scholar 

  12. Billing, F.S.: Shock-wave shapes around spherical -and cylinderical-nosed bodies. J. Spacecr. Rocket. 4(6), 822–833 (1967)

    Article  Google Scholar 

  13. Wu, J.Z.Y.: An organ-pipe oscillation[R]. Imperial college of science and Technology London: 1984

    Google Scholar 

  14. Yuceil, K.B., Dolling, D.S.: Nose cavity effects on blunt body pressure and temperature at Mach 5. J. Thermophys. Heat Transf. 9(4) (1995)

    Google Scholar 

  15. Yuceil, K.B., Dolling, D.S.: IR imaging and shock visualization of flow over a blunt body with a nose cavity. In: 34th Aerospace Sciences Meeting and Exhibit, Reno. (1996)

    Google Scholar 

  16. Engblom, W.A., Yuceil, B., Goldstein, D.B.: Hypersonic forward-facing cavity flow: an experimental and numerical study. In: 33rd Aerospace Sciences Meeting and Exhibit, Reno. (1995)

    Google Scholar 

  17. Juliano, T.J., Segura, R.: Starting issues and forward-facing cavity resonance in a hypersonic quite tunnel. In: 38th Fluid Dynamics Conference and exhibit, Seattle. (2008)

    Google Scholar 

  18. Segura, R: Oscillations in a Forward-Facing Cavity Measured Using Laser-Differential Interferometry in a Hypersonic Quiet Tunnel[D]], West Lafayette. Indiana: Purdue University, (2007)

    Google Scholar 

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Correspondence to Wang Gang .

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Gang, W., Xiao-wei, M., Tao, J., Hong-ming, G., Rong-zong, K., Yan-guang, Y. (2018). Forecasting Method of Shock-Standoff Distance for Forward-Facing Cavity. In: Kontis, K. (eds) Shock Wave Interactions. RaiNew 2017. Springer, Cham. https://doi.org/10.1007/978-3-319-73180-3_7

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  • DOI: https://doi.org/10.1007/978-3-319-73180-3_7

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-73179-7

  • Online ISBN: 978-3-319-73180-3

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