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)
Interactional Aerodynamics of the Single Rotor Helicopter Configuration. Volume II-G. Harmonic Analyses of Airframe Surface Pressure Data, Runs 23-33, Forward Section
1978
211 pages
Report
No indication
English
Scaling and Configuration Effects on Helicopter Rotor Hub Interactional Aerodynamics
Online Contents | 2017
|Scaling and Configuration Effects on Helicopter Rotor Hub Interactional Aerodynamics
AIAA | 2017
|