Grant: Discovery Grants Program - Individual
Royal Military College of Canada
$38,000.00
Discovering the Transition Mechanisms in Fundamental Canonical Flows and in Idealized Propulsion Component Systems
FY 2021-22
Summary
Boundary Layer; Bypass Transition; Crossflow Instability; Direct Numerical Simulation; Freestream Turbulence; Osborne Reynolds Pipe Flow; Rotor-Stator Interaction; Transition from Laminar to Turbulence; Von Karman Rotating Disk Boundary Layer; Wake
Program
Discovery Grants Program - Individual
Recipient
Location
Ontario, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data
As published
Application id
RGPIN-2016-03619
Name nom
Wu, Xiaohua
Department département
Mechanical & Aerospace Engineering
Organization id
30
Institution établissement
Royal Military College of Canada
Province en
Ontario
Province fr
Ontario
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2021
Competition year année de concours
2016
Award amount
38000
Program id
RGPIN
Program name en
Discovery Grants Program - Individual
Program name fr
Programme de subventions à la découverte - individuelles
Group en
Discovery grants programs
Group fr
Programmes de subventions à la découverte
Committee code
1512
Committee name en
Mechanical Engineering
Committee name fr
Génie mécanique
Area of application code
703
Area of application group en
Transportation systems and services
Area of application group fr
Services et systèmes de transport
Area of application en
Aerospace
Area of application fr
Aérospatial
Research subject code
2201
Research subject group en
Fluid mechanics
Research subject group fr
Mécanique des fluides
Research subject en
Turbulence
Research subject fr
Turbulence
Installment
inst:6
Partie
1
Nb partie
6
Application title
Discovering the Transition Mechanisms in Fundamental Canonical Flows and in Idealized Propulsion Component Systems
Keyword
NSERC
Application summary
Boundary Layer; Bypass Transition; Crossflow Instability; Direct Numerical Simulation; Freestream Turbulence; Osborne Reynolds Pipe Flow; Rotor-Stator Interaction; Transition from Laminar to Turbulence; Von Karman Rotating Disk Boundary Layer; Wake
