This report presents work performed under a Cooperative Research Agreement between Virginia Tech and the NASA Langley Research Center. The work involved development of computational techniques for modeling helicopter rotor/airframe aerodynamic interaction. A brief overview of the problem is presented, the modeling techniques are described, and selected example calculations are briefly discussed.
Low Speed Rot or/Fuselage Interactional Aerodynamics
2003
40 pages
Report
Keine Angabe
Englisch
Low Speed Rot or/Fuselage Interactional Aerodynamics
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