FLOW NOISE INSIDE BOUNDARY LAYERS OF BUOYANCY-PROPELLED TEST VEHICLES,
Abstract
Boundary-layer pressure fluctuations were measured at selected points along the surface of a free-rising buoyancy-propelled torpedo-shaped vehicle. The pressure spectra were obtained throughout the band from 200 cps to 30 kcps. The transition region was located and the cross-correlation of noise pressure and shell vibration velocity in the laminar region was determined. Spacetime correlation was obtained for closely spaced transducers to show the lifetime, correlation length, and convection velocity of turbulent distrubances. The effect of finite transducer size on the measured pressure was determined. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1965
- Accession Number
- AD0615507
Entities
People
- C. R. Nisewanger
- F. B. Sperling
Organizations
- Naval Air Weapons Station China Lake