A third and final international project has been completed for the assessment of state-of-the-art computational fluid dynamics (CFD) capabilities to predict flight data obtained with an F-16XL aircraft. This work built upon two prior campaigns associated with the Cranked Arrow-Wing Aerodynamics Project International (CAWAPI). The second CAWAPI project, CAWAPI-2, focused on predictions for low-speed/high-angle-of-attack and transonic/low-to-moderate angle-of-attack conditions, and eight papers from this effort were published in Volume 54, Issue 2, of the Journal of Aircraft.
Introduction to the Special Section on F-16XL Flight Aerodynamics Predictions at a High Angle-of-Attack
2017
3 pages
Report
No indication
English
Introduction to the Special Section on the Prediction of F-16XL In-Flight Aerodynamics
Online Contents | 2017
|SPECIAL SECTION: PREDICTION OF F-16XL FLIGHT-FLOW PHYSICS - Prediction of F-16XL Flight-Flow Physics
Online Contents | 2009
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