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Aerodynamic force measurements over missile configurations in IISc shock tunnel at M∞ = 5.5

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References

  • Muraca, R. J. 1966: An empirical method for determining static distributed aerodynamic loads on axisymmetric multistage launch vehicle. NASA TN D-3283

  • Reddy, N. M. 1983: Aerodynamic force measurements in IISC hypersonic shock tunnel. Proc. of XIV International symposium on shock tubes and shock waves, Sydney, Australia, 358–362

  • Truitt, R. W. 1959: Hypersonic aerodynamics. New York: Ronald Press

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  1. Department of Aerospace Engineering, Indian Institute of Science, 560012, Bangalore, India

    M. V. Joshi & N. M. Reddy

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  1. M. V. Joshi
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  2. N. M. Reddy
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Joshi, M.V., Reddy, N.M. Aerodynamic force measurements over missile configurations in IISc shock tunnel at M∞ = 5.5. Experiments in Fluids 4, 338–340 (1986). https://doi.org/10.1007/BF00266300

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