Effect of Inlet Conditions on the Operation of an Axisymmetric Diffuser,
Abstract
The study deals with the effects of changes in (inlet) boundary layer thickness and on the performance of an axisymmetric diffuser. The test data of this diffuser with an angle of opening of 8 deg. and an L/D (sub a) ratio = 8.83 are included. The volume of displacement at the input is taken as variable and is controlled by the length of the mixer pipe. The test was conducted at a Reynold number within 90,000-400,000. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 03, 1968
- Accession Number
- AD0845114
Entities
People
- Jerzy Miczka
Organizations
- National Air and Space Intelligence Center