• 3468 Citations
  • 32 h-Index
1971 …2020

Research output per year

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Research Output

Open Access

Nonequilibrium effects on prediction of aerothermodynamic loading for a double cone

Kianvashrad, N. & Knight, D. D., 2019, In : AIAA journal. 57, 7, p. 2946-2963 18 p.

Research output: Contribution to journalArticle

  • 1 Scopus citations

    Numerical simulation of laser energy discharge for flight control

    Kianvashrad, N. & Knight, D., Sep 24 2019, In : Journal of Physics D: Applied Physics. 52, 49, 494005.

    Research output: Contribution to journalArticle

  • 1 Scopus citations

    Shock-shock interaction over a hemisphere in hypersonic flow

    Kianvashrad, N. & Knight, D., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • Effect of non-equilibrium model on drag reduction of a hemisphere-cylinder in supersonic flow

    Kianvashrad, N. & Knight, D., Jan 1 2018, 2018 Flow Control Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3757. (2018 Flow Control Conference).

    Research output: Chapter in Book/Report/Conference proceedingConference contribution