THEORETICAL AND EXPERIMENTAL INVESTIGATION OF A HYPERSONIC MULTI-STAGE COMPRESSOR. PART III. AERODYNAMIC AND HEAT TRANSFER ANALYSIS OF A FULL ADMISSION COMPRESSOR,
Abstract
The results of a study of a series of full-admission multi-stage compressors used for generating high temperature air for hypersonic wind tunnels is presented. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1961
- Accession Number
- AD0686440
Entities
People
- Marian Visich Jr.
Organizations
- New York University Tandon School of Engineering