Skip to main navigation
Skip to search
Skip to main content
Technical University of Munich Home
Help & FAQ
Link opens in a new tab
English
Deutsch
Search content at Technical University of Munich
Home
Profiles
Research units
Projects
Research output
Equipment
Prizes
Activities
Press/Media
Numerical simulation of boundary-layer transition at Mach two
N. D. Sandham
,
N. A. Adams
Queen Mary University of London
Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)
Research output
:
Contribution to journal
›
Article
›
peer-review
15
Scopus citations
Overview
Fingerprint
Fingerprint
Dive into the research topics of 'Numerical simulation of boundary-layer transition at Mach two'. Together they form a unique fingerprint.
Sort by
Weight
Alphabetically
Keyphrases
Numerical Simulation
100%
Mach number
100%
Free Stream
100%
Boundary Layer Transition
100%
Two Dimensional
50%
Growth Rate
50%
Direct numerical Simulation
50%
Small Amplitude
50%
Unstable Modes
50%
Streamwise Vortices
50%
Oblique Waves
50%
Linear Stability Theory
50%
Random Initial Conditions
50%
Two-dimensional Wave
50%
Nonlinear Development
50%
Disturbance Waves
50%
Compressible Navier Stokes Equations
50%
Nonlinear Stage
50%
Three-dimensional Disturbances
50%
Engineering
Two Dimensional
100%
Boundary Layer Transition
100%
Computer Simulation
100%
Mach Number
50%
Streamwise
50%
Compressible Navier
50%
Free-Stream Mach Number
50%
Dimensional Disturbance
50%
Linearized Stability
50%
Random Initial Condition
50%
Free Flow
50%
Navier-Stokes Equation
50%
Direct Numerical Simulation
50%