Interactional Aerodynamics of the Single Rotor Helicopter Configuration. Volume II-I. Harmonic Analyses of Airframe Surface Pressure Data, Runs 23-33, Aft Section.
Abstract
This is the ninth 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 aft section of the model. Test conditions here involve speeds from 20 knots to 160 knots in level flight. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1978
- Accession Number
- ADA060870
Entities
People
- Philip F. Sheridan
Organizations
- Boeing Rotorcraft Systems