Separated Flow

132 books
Evaluation of F/A-18A HARV inlet flow analysis with flight dataUnknown Author

Evaluation of F/A-18A HARV inlet flow analysis with flight data

Unknown Author

1995No page data
Unsteady three-dimensional marginal separation, including breakdownPeter W. Duck
⏱ 29m

Unsteady three-dimensional marginal separation, including breakdown

Peter W. Duck

199029 pp.
An analytical model for highly separated flow on airfoils at low speedsGlen W. Zumwalt
⏱ 1h 55m

An analytical model for highly separated flow on airfoils at low speeds

Glen W. Zumwalt

1977115 pp.
Advancement of a method for calculating separated flows around airfoils with special consideration of profile dragKlaus Jacob
⏱ 56m

Advancement of a method for calculating separated flows around airfoils with special consideration of profile drag

Klaus Jacob

197756 pp.
Control of leading-edge separation on an airfoil by localized excitationAlexander Dovgal
⏱ 54m

Control of leading-edge separation on an airfoil by localized excitation

Alexander Dovgal

199354 pp.
Special course on three-dimensional supersonic/hypersonic flows including separationNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 6h 34m

Special course on three-dimensional supersonic/hypersonic flows including separation

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1990394 pp.
Calculation of 3D separated turbulent flows in boundary layer limitNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
⏱ 2h 23m

Calculation of 3D separated turbulent flows in boundary layer limit

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

1990143 pp.
Numerical simulation of the SOFIA flowfieldStephen P. Klotz

Numerical simulation of the SOFIA flowfield

Stephen P. Klotz

1994No page data
Stability of separating subsonic boundary layersJamal A. Masad

Stability of separating subsonic boundary layers

Jamal A. Masad

1994No page data
Photodamage cell selectionH. Herweijer
⏱ 3h 5m

Photodamage cell selection

H. Herweijer

1999185 pp.
Laminar flow cyclone development programGeneral Electric Company. Mechanical Systems and Technology Laboratory. Mechanics Branch

Laminar flow cyclone development program

General Electric Company. Mechanical Systems and Technology Laboratory. Mechanics Branch

1979No page data
Fully nonlinear Gortler vortices in constricted channel flows and their effect on the onset of separationJames P. Denier
⏱ 31m

Fully nonlinear Gortler vortices in constricted channel flows and their effect on the onset of separation

James P. Denier

199231 pp.
The aerodynamics of delta wings of elliptical cross-section with separated flowNikos J. Mourtos
⏱ 53m

The aerodynamics of delta wings of elliptical cross-section with separated flow

Nikos J. Mourtos

198553 pp.
Numerical solutions of the complete Navier-Stokes equationsH. A. Hassan

Numerical solutions of the complete Navier-Stokes equations

H. A. Hassan

1989No page data
A computionally efficient modelling of laminar separation bubblesPaolo Dini

A computionally efficient modelling of laminar separation bubbles

Paolo Dini

1989No page data
Application of viscous-inviscid interaction methods to transonic turbulent flowsD. Lee

Application of viscous-inviscid interaction methods to transonic turbulent flows

D. Lee

1986No page data
Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flowsKhaled S. Abdol-Hamid

Application of Navier-Stokes code PAB3D with k-e turbulence model to attached and separated flows

Khaled S. Abdol-Hamid

1995No page data
Enhanced line integral convolution with flow feature detectionArthur Okada

Enhanced line integral convolution with flow feature detection

Arthur Okada

1996No page data
Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling methodEuromech Colloquium (349th 1996 Göttingen, Germany)

Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method

Euromech Colloquium (349th 1996 Göttingen, Germany)

1996No page data
Analysis of two-equation turbulence models for recirculating flowsS. Thangam
⏱ 20m

Analysis of two-equation turbulence models for recirculating flows

S. Thangam

199120 pp.
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