Grant: Collaborative Research and Development Grants
University of Calgary
$390,845.00
Analysis, Design, Ground and Flight Testing of an Intake System for Transonic Flight
FY 2019-20
Summary
In collaboration with Atlantis Research Labs Inc., the goals of this CRD project are to better understand theflow physics associated with a novel intake concept, leverage the knowledge to design and optimize thesystem, and perform innovative ground- and flight-based tests for validation. The work is motivated by thedevelopment of the Atlantis Intake System (AIS) for high-speed propulsion applications. Applications includesupersonic aircraft, unmanned aerial systems (UAS), missiles, and targets. State-of-the-art simulation modelingwill be used in combination with optimization and design. A high Mach number impulse apparatus will beused in conjunction with advanced non-intrusive diagnostics to obtain experimental validation data. Flighttesting will involve novel use of aircraft. Results will be exploited to improve the AIS design and betterunderstand entrainment from a heated supersonic jet flow. The work will also provide detailed analysis on anew type of propulsion cycle. In addition to the development of the AIS and better understanding of the flowphysics, major contributions from the project also include the training of highly qualified personnel (HQP) andincreasing the exposure of high-tech research in the aerospace field in western Canada.
Program
Collaborative Research and Development Grants
Recipient
Location
Alberta, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data
As published
Application id
518161-2017
Name nom
Johansen, Craig
Department département
Mechanical and Manufacturing Engineering
Organization id
11
Institution établissement
University of Calgary
Province en
Alberta
Province fr
Alberta
Country en
CANADA
Country fr
CANADA
Fiscal year exercice financier
2019
Competition year année de concours
2017
Award amount
390845
Program id
CRDPJ
Program name en
Collaborative Research and Development Grants
Program name fr
Subventions de recherche et développement coopérative
Group en
RESEARCH PARTNERSHIPS
Group fr
PARTENARIATS DE RECHERCHE
Committee code
141
Committee name en
University/Industry
Committee name fr
Universités/industrie
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
2200
Research subject group en
Fluid mechanics
Research subject group fr
Mécanique des fluides
Research subject en
Fluid mechanics
Research subject fr
Mécanique des fluides
Installment
inst:1 - 1
Partie
1
Nb partie
1
Application title
Analysis, Design, Ground and Flight Testing of an Intake System for Transonic Flight
Keyword
NSERC
Application summary
In collaboration with Atlantis Research Labs Inc., the goals of this CRD project are to better understand theflow physics associated with a novel intake concept, leverage the knowledge to design and optimize thesystem, and perform innovative ground- and flight-based tests for validation. The work is motivated by thedevelopment of the Atlantis Intake System (AIS) for high-speed propulsion applications. Applications includesupersonic aircraft, unmanned aerial systems (UAS), missiles, and targets. State-of-the-art simulation modelingwill be used in combination with optimization and design. A high Mach number impulse apparatus will beused in conjunction with advanced non-intrusive diagnostics to obtain experimental validation data. Flighttesting will involve novel use of aircraft. Results will be exploited to improve the AIS design and betterunderstand entrainment from a heated supersonic jet flow. The work will also provide detailed analysis on anew type of propulsion cycle. In addition to the development of the AIS and better understanding of the flowphysics, major contributions from the project also include the training of highly qualified personnel (HQP) andincreasing the exposure of high-tech research in the aerospace field in western Canada.