Boundary Layer Stability Analysis for Stetson’s Mach 6 Blunt Cone Experiments

doi 10.2514/6.2016-0598
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics

Related search

Numerical Simulation of Leading Edge Receptivity of Stetson's Mach 8 Blunt Cone Stability Experiments

2003English

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

2009English

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

2012English

Hypersonic Boundary-Layer Transition Research in the Boeing/Afosr Mach-6 Quiet Tunnel

2006English

Hypersonic Boundary Layer Stability Over a Flared Cone in a Quiet Tunnel

1996English

Parametric Study of Boundary-Layer Receptivity to Freestream Hot-Spot Perturbation Over a Blunt Compression Cone

2014English

A Nonlinear Stability Approach to Boundary-Layer Transition Data Analysis.

1978English

Stability of Hypersonic Boundary-Layer Flows

1997English

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

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

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy