Skip to main navigation
Skip to search
Skip to main content
National Cheng Kung University Home
English
中文
Home
Profiles
Research units
Research output
Projects
Student theses
Equipment
Prizes
Activities
Search by expertise, name or affiliation
Three-dimensional effect on transonic rectangular cavity flows
Kung-Ming Chung
Department of Aeronautics and Astronautics
Aerospace Science and Technology Research Center
Research output
:
Contribution to journal
›
Article
›
peer-review
26
Citations (Scopus)
Overview
Fingerprint
Fingerprint
Dive into the research topics of 'Three-dimensional effect on transonic rectangular cavity flows'. Together they form a unique fingerprint.
Sort by
Weight
Alphabetically
Keyphrases
Rectangular Cavity
100%
Transonic
100%
Three-dimensional Effect
100%
Cavity Flow
100%
Flow Field
33%
Pressure Gradient
33%
Trailing Edge
33%
3D Effects
33%
Mach number
33%
Peak Pressure
33%
Cavity Length
33%
Pressure Fluctuation
33%
Length-to-depth Ratio
33%
Trailing Vortex
33%
Engineering
Cavity Flow
100%
Rectangular Cavity
100%
Trailing Edge
66%
Pressure Gradient
33%
Depth Ratio
33%
Peak Pressure
33%
Mach Number
33%
Cavity Length
33%
Pressure Fluctuation
33%
Rear Face
33%
Edge Vortex
33%