Accession Number:

ADA061361

Title:

Interactional Aerodynamics of the Single Rotor Helicopter Configuration. Volume II-G. Harmonic Analyses of Airframe Surface Pressure Data, Runs 23-33, Forward Section.

Descriptive Note:

Final rept. Mar 77-Feb 78,

Corporate Author:

BOEING VERTOL CO PHILADELPHIA PA

Personal Author(s):

Report Date:

1978-09-01

Pagination or Media Count:

211.0

Abstract:

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

Subject Categories:

  • Helicopters
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE