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Grant: Collaborative Research and Development Grants

University of Calgary

$310,375.00

Analysis, Design, Ground and Flight Testing of an Intake System for Transonic Flight

FY 2024-25

Summary
In collaboration with Atlantis Research Labs Inc., the goals of this CRD project are to better understand the flow physics associated with a novel intake concept, leverage the knowledge to design and optimize the system, and perform innovative ground- and flight-based tests for validation. The work is motivated by the development of the Atlantis Intake System (AIS) for high-speed propulsion applications. Applications include supersonic aircraft, unmanned aerial systems (UAS), missiles, and targets. State-of-the-art simulation modeling will be used in combination with optimization and design. A high Mach number impulse apparatus will be used in conjunction with advanced non-intrusive diagnostics to obtain experimental validation data. Flight testing will involve novel use of aircraft. Results will be exploited to improve the AIS design and better understand entrainment from a heated supersonic jet flow. The work will also provide detailed analysis on a new type of propulsion cycle. In addition to the development of the AIS and better understanding of the flow physics, major contributions from the project also include the training of highly qualified personnel (HQP) and increasing the exposure of high-tech research in the aerospace field in western Canada.
Program
Collaborative Research and Development Grants
Location
Alberta, Canada
Recipient Type
Academia
Type
Grant
Source
NSERC's Awards Data

As published

Application id
518161-2017
Name nom
Johansen, Craig T
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
2024
Competition year année de concours
2017
Award amount
310375
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
Field of research list names en
Not available
Field of research list names fr
Non disponible
Socioeconomic objective list names en
Not available
Socioeconomic objective list names fr
Non disponible
Application title
Analysis, Design, Ground and Flight Testing of an Intake System for Transonic Flight
Keywords
aerodynamics; computational fluid dynamics; intake system; jet; large eddy simulation; non-intrusive diagnostics; paricle image velocimetry; propulsion; schlieren photography; supersonic
Application summary
In collaboration with Atlantis Research Labs Inc., the goals of this CRD project are to better understand the flow physics associated with a novel intake concept, leverage the knowledge to design and optimize the system, and perform innovative ground- and flight-based tests for validation. The work is motivated by the development of the Atlantis Intake System (AIS) for high-speed propulsion applications. Applications include supersonic aircraft, unmanned aerial systems (UAS), missiles, and targets. State-of-the-art simulation modeling will be used in combination with optimization and design. A high Mach number impulse apparatus will be used in conjunction with advanced non-intrusive diagnostics to obtain experimental validation data. Flight testing will involve novel use of aircraft. Results will be exploited to improve the AIS design and better understand entrainment from a heated supersonic jet flow. The work will also provide detailed analysis on a new type of propulsion cycle. In addition to the development of the AIS and better understanding of the flow physics, major contributions from the project also include the training of highly qualified personnel (HQP) and increasing the exposure of high-tech research in the aerospace field in western Canada.