Flowfield in the vicinity of cylindrical protuberances on a flat plate in supersonic flow.

PAUL J. WALTRUP; DOUGLAS G. HALL; JOSEPH A. SCHETZ

doi:10.2514/3.29203

Flowfield in the vicinity of cylindrical protuberances on a flat plate in supersonic flow.

Journal of Spacecraft and Rockets ◽

10.2514/3.29203 ◽

1968 ◽

Vol 5 (1) ◽

pp. 127-128 ◽

Cited By ~ 11

Author(s):

PAUL J. WALTRUP ◽

DOUGLAS G. HALL ◽

JOSEPH A. SCHETZ

Keyword(s):

Supersonic Flow ◽

Flat Plate

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Efficiency of plasma actuator ionization in shock wave modification in a rarefied supersonic flow over a flat plate

10.1063/1.4902722 ◽

2014 ◽

Cited By ~ 2

Author(s):

Romain Joussot ◽

Viviana Lago ◽

Jean-Denis Parisse

Keyword(s):

Shock Wave ◽

Supersonic Flow ◽

Flat Plate ◽

Plasma Actuator

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Stability of a wake behind a flat plate in a supersonic flow

Journal of Applied Mechanics and Technical Physics ◽

10.1007/bf02369380 ◽

1995 ◽

Vol 36 (6) ◽

pp. 844-847

Author(s):

V. I. Lysenko ◽

N. V. Semenov

Keyword(s):

Supersonic Flow ◽

Flat Plate

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Numerical investigation of boundary-layer instabilities over a blunt flat plate at angle of attack in supersonic flow

Notes on Numerical Fluid Mechanics (NNFM) - New Results in Numerical and Experimental Fluid Mechanics ◽

10.1007/978-3-322-86573-1_13 ◽

1997 ◽

pp. 103-110 ◽

Cited By ~ 3

Author(s):

Guido Dietz ◽

Alexander Meijering

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Flat Plate ◽

Numerical Investigation ◽

Angle Of Attack

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Quantification of the effect of surface heating on shock wave modification by a plasma actuator in a low-density supersonic flow over a flat plate

Experiments in Fluids ◽

10.1007/s00348-015-1970-2 ◽

2015 ◽

Vol 56 (5) ◽

Cited By ~ 16

Author(s):

Romain Joussot ◽

Viviana Lago ◽

Jean-Denis Parisse

Keyword(s):

Shock Wave ◽

Supersonic Flow ◽

Flat Plate ◽

Plasma Actuator ◽

Surface Heating ◽

Low Density ◽

Effect Of Surface

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Experimental and numerical studies of supersonic flow over circular protuberances on a flat plate

Acta Physica Sinica ◽

10.7498/aps.64.054705 ◽

2015 ◽

Vol 64 (5) ◽

pp. 054705

Author(s):

Gang Dun-Dian ◽

Yi Shi-He ◽

Zhao Yun-Fei

Keyword(s):

Supersonic Flow ◽

Flat Plate ◽

Numerical Studies

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Supersonic Cascade Interaction

Volume 1A: General ◽

10.1115/74-gt-76 ◽

1974 ◽

Cited By ~ 1

Author(s):

H. J. Lichtfuss ◽

H. Starken

Keyword(s):

Exact Solution ◽

Supersonic Flow ◽

Flat Plate ◽

Constant Velocity ◽

Flow Conditions ◽

Inlet Flow ◽

Flow Adjustment ◽

Outlet Flow ◽

Quantitative Results ◽

Cascade Interaction

The supersonic flow adjustment between two interacting blade rows is predicted theoretically. One of both cascades may have a constant velocity in the circumferential direction. The calculation is carried out in a quasi-stationary manner. This represents an exact solution if the constant inlet and outlet flow conditions are solely under the scope of view. Admitting the above assumptions it is possible to calculate the uniform outlet flow of the first and the associated inlet flow of the second cascade as a function of the circumferential velocity. Quantitative results are presented for flat plate cascades. However, the method is not at all restricted to these simple cases.

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