Computation of turbulent incompressible wing-body junction flow

Burke, Roger

doi:10.2514/6.1989-279

Cited by 9 publications

(2 citation statements)

References 4 publications

Supporting

Mentioning

Contrasting

Order By: Relevance

“…Chang and Gessner [18] and Fleming et al [23] measured the characteristics of the turbulent flow in the vicinity and downstream of the wing-body junction. For the analysis of the subsonic flow in wing-body junctions, Navier-Stokes flow solvers have been applied successfully by Burke [17] and Paul and Carlson [36].…”

Section: Subsonic 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

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: Subsonic 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

“…Bleev's mixing length21) for the open corner formed by the normal intersection of two planes is used for the present study. ( 9 ) When the open corner has an arbitrary intersection angle 0, more general formula19) for characteristic length 1 is given by…”

Section: Turbulence Modelmentioning

confidence: 99%

Turbulent Flow around an Inclined Strut Mounted on a Plate and Effects of the Angle of Attack

Kim

Mori

1993

J. SNAJ, Nihon zousen gakkai ronbunshu

View full text Add to dashboard Cite

A numerical study on the turbulent flow around the strut-plate juncture is carried out for the inclined strut and for the flow with an angle of attack. Computations are made by solving three-dimensional . incompressible Reynolds-averaged Navier-Stokes equation with MAC method . Turbulence is simulated by using Baldwin-Lomax model with a modified length scale for the treatment of corner flow . The flows, at the Reynolds number of 105, show intensive unsteady behavior near the plate while the flows are steady enough off the plate. Inclination of the strut induces a lift which is generated mainly near the plate. On the other hand, the lift by an angle of attack reduces near the plate .

show abstract

Navier‐Stokes computations of horseshoe vortex flows

Deng

Piquet

1992

Numerical Methods in Fluids

View full text Add to dashboard Cite

SUMMARYThe computation of the incompressible three-dimensional turbulent viscous flow about an aerofoil/flat plate junction is investigated. An iterative, fully decoupled technique is applied to the Reynolds-averaged Navier-Stokes equations (RANSEs) written in a non-orthogonal curvilinear body-fitted co-ordinate system. The results of the computations are compared with well-documented experiments.

show abstract

Computation of turbulent incompressible wing-body junction flow

Cited by 9 publications

References 4 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

Turbulent Flow around an Inclined Strut Mounted on a Plate and Effects of the Angle of Attack

Navier‐Stokes computations of horseshoe vortex flows

Contact Info

Product

Resources

About