Peter W. Duck · National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering

Sayfa sayısı yok · 1991

Boundary layer / Flow velocity / Free flow / Laminar boundary layer / Circular cylinders

Shock wavesOn the interactions between the shock wave attached to a wedge and freestream disturbancesPeter W. Duck

On the interactions between the shock wave attached to a wedge and freestream disturbances

Peter W. Duck · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1993

Shock waves

Supersonic AerodynamicsNonaxisymmetric viscous lower branch modes in axisymmetric supersonic flowsPeter W. Duck

Nonaxisymmetric viscous lower branch modes in axisymmetric supersonic flows

Peter W. Duck · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1988

Aerodynamics, Supersonic / Supersonic Aerodynamics

Boundary layerThe response of a laminar boundary layer in supersonic flow to small amplitude progressive wavesPeter W. Duck

The response of a laminar boundary layer in supersonic flow to small amplitude progressive waves

Peter W. Duck · National Aeronautics and Space Administration

Sayfa sayısı yok · 1989

Boundary layer

Flows (Differentiable dynamical systems)On the linear stability of compressible plane couette flowPeter W. Duck

On the linear stability of compressible plane couette flow

Peter W. Duck · National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering

Sayfa sayısı yok · 1991

Stability / Flows (Differentiable dynamical systems)

Shock wavesOn the interaction between the shock wave attached to a wedge and freestream disturbancesPeter W. Duck

On the interaction between the shock wave attached to a wedge and freestream disturbances

Peter W. Duck · Institute for Computer Applications in Science and Engineering

44 sayfa · 1993

Free flow / Shock waves

Flow stabilityThe inviscid stability of supersonic flow past a sharp conePeter W. Duck

The inviscid stability of supersonic flow past a sharp cone

Peter W. Duck · National Technical Information Service, distributor

Sayfa sayısı yok · 1990

Inviscid flow / Mathematical models / Supersonic flow / Cones / Flow stability