Favorable interference of optimized wing-body combination with inlet at supersonic speed

Pritulo, T; Gubanov, Anatoly; Voevodenko, Nina

doi:10.2514/6.1995-3946

Cited by 1 publication

(1 citation statement)

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“…The Navier-Stokes solutions of Lakshmanan and Tiwari [85] showed that, by properly filleting the junction between a swept fin and a flat One application of the study of the flow around a fin perpendicular to a flat wall is the design of wing-fuselage junctions. Favorable aerodynamic interference was achieved between the wing and the fuselage by Pritulo et al [89]. The shape of the wing-body combination was determined by employing an Euler flow solver and applying simple surface deformations to the existing geometry.…”

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

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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.

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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

Favorable interference of optimized wing-body combination with inlet at supersonic speed

Cited by 1 publication

References 1 publication

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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