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Acharya, A., & Rao, S. S. (2023). Vortex Breakdown Study and Developing a Pitch up Delay on A Generic Single Engine Delta Winged Fighter Using Along The Core Axis Jet Blowing. Journal of Aerospace Sciences and Technologies, 75(2), 203–207. https://doi.org/10.61653/joast.v75i2.2023.62

References

  1. Yip, L. P. and Parlett, L. P., "Low-Speed Wind-Tunnel Tests of a 1/10-Scale Model of an Arrow-Wing Supersonic Cruise Configuration Designed for Cruise at Mach 2.2", 1979, NASA TM 80152.
  2. Carlson, H. W., Darden, C. M. and Mann, M. J., "Validation of a Computer Code for Analysis of Subsonic Aerodynamic Performance of Wings with Flaps in Combination with a Canard or Horizontal Tail and an Application to Optimization", 1990, NASA TP 2961.
  3. Anand Kumar., "On the Structure of Vortex Breakdown on a Delta Wing", Mathematical, Physical and Engineering Sciences, The Royal Society, Vol.454, No.1968, 1997, pp.89-110.
  4. Rao, D. M., "Exploratory Investigation of a Tip Blowing Concept on a Cranked-Arrow HSCT Planform", 10th Applied Aerodynamics Conference, The American Institute of Aeronautics and Astronautics, 1992.
  5. Anthony Mitchell., Scott Morton., Pascal Molton and Yair Guy., "Flow Control of Vortical Structures and Vortex Breakdown Over Slender Delta Wings", RTO-MP-069(I), 2001.
  6. Schmucker, A. and Gersten, K., "Vortex Breakdown and its Control on Delta Wings", Fluid Dynamics Research 3, 1988, pp. 268-272.

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