Interactional Aerodynamics of the Single Rotor Helicopter Configuration. Volume II-G. Harmonic Analyses of Airframe Surface Pressure Data, Runs 23-33, Forward Section.
Final rept. Mar 77-Feb 78,
BOEING VERTOL CO PHILADELPHIA PA
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This is the seventh of the nine sub-volumes of Volume II. These documents contain harmonic analyses of the waveforms generated by each of the 53 pressure transducers, which covered the surface of the model fuselage and empennage. This sub-volume covers the final eleven of the twenty-seven runs devoted to surface pressure testing. The analyses encompass the transducers in the forward section of the model. Test conditions here involve speeds from 20 knots to 160 knots in level flight. Author
- Fluid Mechanics