Prediction of Rotor/Propeller Rotational Noise,
Abstract
An analysis of the rotational noise sound field of a rotor/propeller has been carried out. The resulting equations have been programmed on an IBM-360 computer. The program has been successfully checked out by comparison with existing theory. Also, a short parametric study has been carried out as part of the computer program evaluation.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 20, 1968
- Accession Number
- AD0785929
Entities
People
- G. J. Healy
Organizations
- Lockheed Martin