HELICOPTER ROTOR NOISE ANALYSIS.
Abstract
A preliminary analytical method for predicting whether rotor blade bang will occur is described and correlated with data from tandem rotor helicopters. The operating limits which will cause banging of a single rotor are discussed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 22, 1966
- Accession Number
- AD0684036
Entities
People
- E. G. Schaeffer
Organizations
- Boeing Rotorcraft Systems