The impact of a shock-wave on a thin two-dimensional aerofoil moving at supersonic speed
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Publication:3850743
DOI10.1017/S0022112063000197zbMath0112.18801OpenAlexW2170629086MaRDI QIDQ3850743
Publication date: 1963
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/s0022112063000197
Related Items (12)
Diffraction of a shock wave on a wedge moving at supersonic speed ⋮ Supersonic flow over a thin wedge intersected by the front of an external plane compression shock ⋮ Normal shock interaction with a yawed wedge moving at supersonic speed ⋮ Reflection of a rightward-moving oblique shock of first family over a steady oblique shock wave ⋮ Plane nonstationary self-similar gas flow with energy liberation in shock waves ⋮ Shock wave diffraction on a thin wedge moving with a slip relative to the wave front with irregular shock interaction ⋮ Antisymmetric problems in shock diffraction theory ⋮ Diffraction of a shock wave on a wedge moving at supersonic velocity ⋮ Diffraction of a shock wave on a thin wedge moving at supersonic speed under the conditions of sporadic wave interaction ⋮ Integral transforms for shock-shock interaction - Three dimensional planar wings ⋮ Diffraction of a plane wave by a wedge moving with supersonic speed ⋮ Reflection of rightward moving shocks of the first and second families over a steady oblique shock wave
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