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5 research outputs found

Control of shock-wave boundary-layer interactions by bleed in supersonic mixed compression inlets

Author: Anderson B.H..
Cubbison R. W.
Cubbison R.W..
Fukuda M.K.
Hcldfferty C.
Kilburg R.P.
Seebaugh W. R.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
Publication date
Field of study

A fast, uncoupled, compressible, two-dimensional, unsteady boundary layer algorithm with separation for engine inlets

Author: Cpbeci T.
Cubbison R.W.
Davis R.T.
Lewis J.E.
Sakowski B.A.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
Publication date
Field of study

Secondary Gas Injection into a Supersonic Conical Nozzle

Author: Cubbison R.W.
Goro Masuya
Nobuo Chinzei
Rogers R.C.
Shinichi Ishii
Torrence M.G.
Wagner J.P.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
Publication date
Field of study

Development of a coupled inlet-engine dynamic analysis method

Author: Choby D.
Colella P.
Cubbison R.W.
Figure
Garrard D.
Mayer D.W.
Mayer D.W.
McLafferty G.H.
Paynter G.C.
Strang W.Z.
Williamson J.H.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
Publication date
Field of study

Pressure-Sensitive Paint Measurements of Sonic Jet Injection into Supersonic Crossflow

Author: Ashkenas H.
Bowersox R. D. W.
Cubbison R.W.
Everett D.E.
Gruber M. R.
Kameda M.
Sakamura Y.
Sakaue H.
Viti W.
Publication venue: 'American Institute of Aeronautics and Astronautics (AIAA)'
Publication date
Field of study

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