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1

Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow

Settles, Gary S., Fitzpatrick, Thomas J., Bogdonoff, Seymour M.

Journal:

Year:

1979

Language:

english

File:

PDF, 1.09 MB

english, 1979

2

Incipient Separation of a Supersonic Turbulent Boundary Layer at High Reynolds Numbers

Settles, Gary S., Bogdonoff, Seymour M., Vas, Irwin E.

Journal:

Year:

1976

Language:

english

File:

PDF, 1021 KB

english, 1976

3

Radiatively driven hypersonic wind tunnel

Miles, Richard B., Brown, Garry L., Lempert, Walter R., Yetter, Richard, Williams, George J., Bogdonoff, Seymour M., Natelson, Douglas, Guest, Jeffrey R.

Journal:

Year:

1995

Language:

english

File:

PDF, 1.07 MB

english, 1995

4

ro

Settles, Gary S., Vas, Irwin E., Bogdonoff, Seymour M.

Journal:

Year:

1976

Language:

english

File:

PDF, 957 KB

english, 1976

5

[American Institute of Aeronautics and Astronautics 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference - Honolulu,HI,U.S.A. (08 June 1987 - 10 June 1987)] 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference - A comparative experimental investigation of shock/turbulent boundarylayer interactions produced by three shock generators

BOGDONOFF, SEYMOUR

Year:

1987

Language:

english

File:

PDF, 677 KB

english, 1987

6

[American Institute of Aeronautics and Astronautics 26th Aerospace Sciences Meeting - Reno,NV,U.S.A. (11 January 1988 - 14 January 1988)] 26th Aerospace Sciences Meeting - Supersonic turbulent flow past a swept compression corner at Mach 3.II

KNIGHT, DOYLE, HORSTMAN, C., BOGDONOFF, SEYMOUR

Year:

1988

Language:

english

File:

PDF, 802 KB

english, 1988

7

[American Institute of Aeronautics and Astronautics 28th Aerospace Sciences Meeting - Reno,NV,U.S.A. (08 January 1990 - 11 January 1990)] 28th Aerospace Sciences Meeting - The modeling of a three-dimensional shock wave turbulent boundary layer interaction - The Dryden Lectureship

BOGDONOFF, SEYMOUR

Year:

1990

Language:

english

File:

PDF, 1.05 MB

english, 1990

8

[American Institute of Aeronautics and Astronautics 29th Joint Propulsion Conference and Exhibit - Monterey,CA,U.S.A. (28 June 1993 - 30 June 1993)] 29th Joint Propulsion Conference and Exhibit - Time-sequenced and spectrally filtered Rayleigh imaging of shock wave and boundary layer structure for inlet characterization

FORKEY, JOSEPH, COGNE, SANDRINE, SMITS, ALEXANDER, BOGDONOFF, SEYMOUR, LEMPERT, WALTER, MILES, RICHARD

Year:

1993

Language:

english

File:

PDF, 627 KB

english, 1993

9

Structure of supersonic turbulent flow past a sharp fin

KNIGHT, DOYLE D., HORSTMAN, C., BOGDONOFF, SEYMOUR, SHAPEY, BRIAN

Journal:

Year:

1987

Language:

english

File:

PDF, 844 KB

english, 1987

10

Investigation of Three-Dimensional Shock/Boundary-Layer Interactions at Swept Compression Corners

Settles, Gary S., Perkins, Jeffrey J., Bogdonoff, Seymour M.

Journal:

Year:

1980

Language:

english

File:

PDF, 1.06 MB

english, 1980

11

Structure of supersonic turbulent flow past a swept compression corner

KNIGHT, DOYLE D., HORSTMAN, C., BOGDONOFF, SEYMOUR

Journal:

Year:

1992

Language:

english

File:

PDF, 916 KB

english, 1992

12

Scaling of Two- and Three-Dimensional Shock/Turbulent Boundary-Layer Interactions at Compression Corners

Settles, Gary S., Bogdonoff, Seymour M.

Journal:

Year:

1982

Language:

english

File:

PDF, 1.08 MB

english, 1982

13

SEVENTIETH ANNIVERSARY ISSUE || 200 Miles Upby J. Gorden Vaeth

Review by: Seymour M. Bogdonoff

Journal:

American Scientist

Year:

1957

Language:

english

File:

PDF, 358 KB

english, 1957

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