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Fingerprint Dive into the research topics where Doyle Knight is active. These topic labels come from the works of this person. Together they form a unique fingerprint.

  • 1 Similar Profiles
Mach number Engineering & Materials Science
Boundary layers Engineering & Materials Science
Shock waves Engineering & Materials Science
turbulent boundary layer Physics & Astronomy
Supersonic flow Engineering & Materials Science
shock waves Physics & Astronomy
Navier Stokes equations Engineering & Materials Science
Hypersonic aerodynamics Engineering & Materials Science

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Research Output 1971 2019

Nonequilibrium effects on prediction of aerothermodynamic loading for a double cone

Kianvashrad, N. & Knight, D., Jan 1 2019, In : AIAA journal. 57, 7, p. 2946-2963 18 p.

Rutgers, The State University

Research output: Contribution to journalArticle

Thermochemistry
Cones
Energy transfer
Heat transfer
Hypersonic aerodynamics

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.

Rutgers, The State University

Research output: Contribution to journalArticle

flight control
pitching moments
drag reduction
Drag reduction
Lasers

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).

Rutgers, The State University

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

Hypersonic flow
Strouhal number
Heat transfer
Mach number
Tunnels

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).

Rutgers, The State University

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

drag reduction
supersonic flow
thermochemistry
gas dynamics
hemispheres
3 Citations (Scopus)

Effect of off-body laser discharge on drag reduction of hemisphere cylinder in supersonic flow-part II

Kianvashrad, N., Knight, D., Wilkinson, S. P., Chou, A., Beeler, G. B. & Jangda, M., Jan 1 2018, AIAA Aerospace Sciences Meeting. 210059 ed. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Aerospace Sciences Meeting, 2018; no. 210059).

Rutgers, The State University

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

Drag reduction
Supersonic flow
Discharge (fluid mechanics)
Lasers
Mach number