Measurements of a Supersonic Favorable-Pressure-Gradient Turbulent Boundary Layer with Heat Transfer. Part 1. Data Compilation.
Abstract
The results of a detailed experimental investigation of the compressible turbulent boundary layer in a favorable-pressure-gradient flow are presented for zero, moderate and severe heat-transfer conditions. The studies were conducted on a flat nozzle wall at momentum thickness Reynolds numbers from 6,700 to 56,000 and at three wall-to-adiabatic-wall temperature ratios. An attempt was made to hold values of Clauser's pressure-gradient parameter constant. Complete profile measurements were taken with Pitot pressure probes and conical-equilibrium and fine-wire temperature probes. (Modified author abstract)
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 12, 1973
- Accession Number
- AD0778306
Entities
People
- Robert L. P. Voisinet
- Roland E. Lee
Organizations
- Naval Ordnance Laboratory