AN ANALYTIC SOLUTION TO THE SOUND PRESSURE FIELD RESULTING FROM A PLANE WAVE INCIDENT ON A CYLINDER AND CONCENTRIC CYLINDRICAL SECTION - COMPUTATIONAL TECHNIQUES
Abstract
The computational techniques are described which are used in the numerical evaluation of a solution to the sound pressure field resulting from a plane wave incident on a cylinder and concentric cylindrical section.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 08, 1963
- Accession Number
- AD0406092
Entities
People
- Alice M. Spitzer
- G. S. Mills
- W. C. Moyer
Organizations
- Tracor