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P. R. Ashill

  • A novel technique for controlling shock strength of laminar-flow aerofoil sectionsA novel technique for controlling shock strength of laminar-flow aerofoil sections
  • A study of flows over highly-swept wings designed for manoeuvre at supersonic speedsA study of flows over highly-swept wings designed for manoeuvre at supersonic speeds
  • A study of the flow around the leading edge of a highly-swept wing in a low-speed wind tunnelA study of the flow around the leading edge of a highly-swept wing in a low-speed wind tunnel
  • Boundary-flow measurement for wall interference assessment and correction - classification and reviewBoundary-flow measurement for wall interference assessment and correction - classification and review
  • Calculation and measurement of transonic flows over aerofoils with novel rear sectionsCalculation and measurement of transonic flows over aerofoils with novel rear sections
  • Calibration of the flow in the channel of the whirling armCalibration of the flow in the channel of the whirling arm
  • Control of leading-edge separation on a cambered delta wingControl of leading-edge separation on a cambered delta wing
  • Leading edge flows on highly swept wingsLeading edge flows on highly swept wings
  • Wind tunnel experiments on aerofoil models for the assessment of computational flow methodsWind tunnel experiments on aerofoil models for the assessment of computational flow methods