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Toward improved CFD predictions of slender airframe aerodynamics using the F-16XL aircraft (CAWAPI-2)
- Luckring, J M (author)
-
- Rizzi, Arthur (author)
- KTH,Farkost och flyg
- Bruce Davis, M (author)
- (creator_code:org_t)
- 2014-01-10
- 2014
- English.
- In: 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014. - Reston, Virginia : American Institute of Aeronautics and Astronautics Inc..
- Conference paper (peer-reviewed)
Abstract
Subject headings
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- A coordinated project has been underway to improve CFD predictions of slender airframe aerodynamics. The work is focused on two flow conditions and leverages a unique flight data set obtained with an F-16XL aircraft. These conditions, a low-speed high angle-of-attack case and a transonic low angle-of-attack case, were selected from a prior prediction campaign wherein the CFD failed to provide acceptable results. In this paper the background, objectives and approach to the current project are presented. The work embodies predictions from multiple numerical formulations that are contributed from multiple organizations, and the context of this campaign to other multi-code, multi-organizational efforts is included. The relevance of this body of work toward future supersonic commercial transport concepts is also briefly addressed.
Subject headings
- TEKNIK OCH TEKNOLOGIER -- Maskinteknik -- Rymd- och flygteknik (hsv//swe)
- ENGINEERING AND TECHNOLOGY -- Mechanical Engineering -- Aerospace Engineering (hsv//eng)
Keyword
- Airframes
- Angle of attack
- Angle of attack indicators
- Aviation
- Computational fluid dynamics
- Current projects
- F-16XL aircraft
- Flight data
- Flow condition
- Forecasting
- High angle of attack
- Multiple organizations
- Numerical formulation
- Research aircraft
- Structural frames
- Supersonic aircraft
- Supersonic commercial transports
Publication and Content Type
- ref (subject category)
- kon (subject category)
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- Royal Institute of Technology
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