Skip to main navigation
Skip to search
Skip to main content
Experts@Minnesota Home
Search content at Experts@Minnesota
Home
Profiles
Research units
University Assets
Projects and Grants
Research output
Datasets
Press/Media
Activities
Fellowships, Honors, and Prizes
Impacts
A numerical method for predicting hypersonic flowfields
Robert W. Maccormack
,
Graham V. Candler
Aerospace Engineering and Mechanics
Research output
:
Contribution to journal
›
Article
›
peer-review
Overview
Fingerprint
Fingerprint
Dive into the research topics of 'A numerical method for predicting hypersonic flowfields'. Together they form a unique fingerprint.
Sort by
Weight
Alphabetically
Keyphrases
Hypersonic
100%
Numerical Methods
100%
Flow Field
100%
Thermal Non-equilibrium
33%
Fluid Flow
33%
Dissociation
33%
Vibrational Temperature
33%
Source Term
33%
Energy Transfer
33%
Rate Equations
33%
Hypersonic Speed
33%
Conservation Equations
33%
Viscous Terms
33%
Energy Relations
33%
Temperature State
33%
Matrix Equation
33%
Fluid Flow Equation
33%
Block Matrix
33%
Fully Implicit Method
33%
Central Difference
33%
Atmospheric Gases
33%
Inviscid Flow
33%
Species Formation
33%
Gas Chemistry
33%
Gas Physics
33%
Gauss-Seidel
33%
Physics
Hypersonics
100%
Mathematical Method
100%
Fluid Flow
66%
Chemistry
66%
Energetics
33%
Flux Method
33%
Gas Physics
33%
Atmospherics
33%
Flow Equation
33%
Inviscid Flow
33%
Hypersonic Speed
33%
Energy Relation
33%