A METHOD OF LIQUID JET BLOWOUT UNDER HIGH PRESSURE
Abstract
A hydropneumatic apparatus which has a liquid jet blowout at a velocity of 2000 m/sec and higher is described below. Experimental data on measuring the velocity of turbine oil up to 1850 m/sec is submitted.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 24, 1964
- Accession Number
- AD0600817
Entities
People
- A. A. Semerchan
- M. A. Plotnikov
Organizations
- Air Force Systems Command