Skip to main navigation
Skip to search
Skip to main content
Illinois Experts Home
LOGIN & Help
Home
Profiles
Research units
Research & Scholarship
Datasets
Honors
Press/Media
Activities
Search by expertise, name or affiliation
Spanwise variations in profile drag for airfoils at low reynolds numbers
James J. Guglielmo
,
Michael S. Selig
Aerospace Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
Overview
Fingerprint
Fingerprint
Dive into the research topics of 'Spanwise variations in profile drag for airfoils at low reynolds numbers'. Together they form a unique fingerprint.
Sort by
Weight
Alphabetically
Keyphrases
Low Reynolds number
100%
Span-wise
100%
Airfoil
100%
Profile Drag
100%
Trailing Edge
50%
Wake Profile
50%
Three-dimensional (3D)
25%
Flow Field
25%
Measurement Techniques
25%
Zigzag
25%
Reynolds number
25%
Profile Measurement
25%
Three-dimensionality
25%
Wind Tunnel
25%
Drag Coefficient
25%
Two-dimensional Flow
25%
Chord Length
25%
Angle of Attack
25%
High Reynolds number
25%
Wake Survey
25%
Roughness Element
25%
Tunnel Facility
25%
Drag Measurement
25%
Airfoil Model
25%
Boundary Layer Trips
25%
Isolated Roughness
25%
Spanwise Distance
25%
Laminar Separation Bubble
25%
Engineering
Airfoil
100%
Profile Drag
100%
Trailing Edge
50%
Illustrates
25%
Good Agreement
25%
Two Dimensional
25%
Reynolds' Number
25%
Dimensionality
25%
Boundary Layer
25%
Extreme Case
25%
Drag Coefficient
25%
Dimensional Flow
25%
Chord Length
25%
Angle-of-Attack
25%
High Reynolds Number
25%
Roughness Element
25%
Layer Trip
25%
Laminar Separation Bubble
25%
Tunnel
25%
Earth and Planetary Sciences
Airfoil
100%
Trailing Edge
66%
Wind Tunnels
33%
Reynolds Number
33%
Boundary Layer
33%
High Reynolds Number
33%
Two Dimensional Flow
33%
Drag Measurement
33%