Interactional Aerodynamics of the Single Rotor Helicopter Configuration. Volume II-A. Harmonic Analyses of Airframe Surface Pressure Data, Runs 7-14, Forward Section.
Final rept. Mar 77-Feb 78,
BOEING VERTOL CO PHILADELPHIA PA
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This is the first 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 first eight of the twenty-seven runs devoted to surface pressure testing. The analyses encompass the transducers in the forward section of the model. Test conditions and configurations include baseline data, climb and descent, disk loading variation, and application of strakes. Author
- Fluid Mechanics