Experimental and numerical investigation of supersonic turbulent flow in an annular duct

Williams, K. E.; Gessner, F. B.; Harloff, G. J.

doi:10.2514/6.1993-3123

Cited by 1 publication

(2 citation statements)

References 16 publications

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“…Williams et al [92,91,90,93] performed several numerical and experimental studies about the interference produced by struts in an annular duct in supersonic flow. Those analyses serve as applications to engine development.…”

Section: Supersonic Flowmentioning

confidence: 99%

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Numerical prediction of the interference drag of a streamlined strut intersecting a surface in transonic flow

Tetrault

2000

38th Aerospace Sciences Meeting and Exhibit

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In transonic flow, the aerodynamic interference that occurs on a strut-braced wing airplane, pylons, and other applications is significant. The purpose of this work is to provide relationships to estimate the interference drag of wing-strut, wing-pylon, and wing-body ar- his office, leaving with more answers than questions. I also appreciate the fact that he has always had a friendly attitude towards me. I have enjoyed interacting with Dr. Kapania, whose cheerful attitude and perpective on life and research is very similar to mine. I would like to acknowledge the contribution of Dr. Grossman to the team in the field of numerical calculations and his desire of improving the life of the graduate students by forming the Graduate Advisory Committee. Dr. Raj deserves a lot of thanks for providing me with useful advice throughout this project despite his busy schedule. I appreciate the fact that he has always been interested in knowing more about the evolution of my research work and career. The "virtual" presence of Dr. Haftka during our weekly meetings has been very beneficial because of his ability to foresee difficulties and to get the team members to not lose sight of the big picture.

show abstract

Section: Supersonic Flowmentioning

confidence: 99%

“…Ref. [90] reported the numerical and experimental investigations of the turbulent boundary layer that develops along the side walls of an annular duct.…”

Section: Supersonic Flowmentioning

confidence: 99%

Numerical prediction of the interference drag of a streamlined strut intersecting a surface in transonic flow

Tetrault

2000

38th Aerospace Sciences Meeting and Exhibit

View full text Add to dashboard Cite

show abstract

Experimental and numerical investigation of supersonic turbulent flow in an annular duct

Cited by 1 publication

References 16 publications

Numerical prediction of the interference drag of a streamlined strut intersecting a surface in transonic flow

Numerical prediction of the interference drag of a streamlined strut intersecting a surface in transonic flow

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