Direct Numerical Simulation of Hypersonic Boundary-Layer Transition Over Blunt Leading Edges. I - A New Numerical Method and Validation

doi 10.2514/6.1997-755
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Direct Numerical Simulation on the Receptivity, Instability, and Transition of Hypersonic Boundary Layers

Annual Review of Fluid Mechanics
Condensed Matter Physics
2012English

Numerical Computations of Hypersonic Boundary Layer Roughness Induced Transition on a Flat Plate

2012English

Numerical Simulation of Graphite Ablation Induced Outgassing Effects on Hypersonic Boundary Layer Receptivity Over a Cone Frustum

2013English

Direct Numerical Simulation of Flow Transition Over a Flat Plate

2004English

Direct Numerical Simulation of Flow Past a Sphere in a Plane Turbulent Boundary Layer With Immersed Boundary Method

2012English

Direct Numerical Simulation of a Supersonic Turbulent Boundary Layer at Mach 2.5

Journal of Fluid Mechanics
Mechanics of MaterialsCondensed Matter PhysicsMechanical Engineering
2000English

Linear Stability Study of Hypersonic Boundary Layer Transition on Blunt Circular Cones

2009English

Parametric Geometry Models for Hypersonic Aircraft Components: Blunt Leading Edges

2015English

Experiments on Hypersonic Boundary Layer Transition on Blunt Cones With Acoustic-Absorption Coating

2012English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy