Flowfield in the vicinity of an F/A-18 vertical fin at high angles of attack
Author:
Affiliation:
1. Institute for Aerospace Research, Ottawa, Ontario K1A OR6, Canada
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46307
Reference8 articles.
1. Wind-tunnel studies of F/A-18 tail buffet
2. Statistical prediction of maximum buffet loads on the F/A-18 vertical fin
3. A method for predicting wing response to buffet loads
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1. History of the NRC 1.5m Trisonic Wind Tunnel;AIAA SCITECH 2023 Forum;2023-01-19
2. Visualization of impingement of broken-down vortex on tail;Journal of Wind Engineering and Industrial Aerodynamics;2003-01
3. Pressure Measurements Onboard a Small-Scale Rotating Wind Tunnel Model for Jet/Fin Interaction;22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2002-06-24
4. Statistical analysis of wing/fin buffeting response;Progress in Aerospace Sciences;2002-05
5. VORTEX BREAKDOWN FROM A PITCHING DELTA WING INCIDENT UPON A PLATE: FLOW STRUCTURE AS THE ORIGIN OF BUFFET LOADING;Journal of Fluids and Structures;2002-04
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