TABULATED FORCE AND MOMENT DATA FOR A SERIES OF CIRCULAR, ANNULAR JET GROUND EFFECT MACHINE MODELS
Abstract
Wind tunnel were conducted on 9 circular, annular jet, ground effect machine models. The effects of slot width, convergence angle of the jet and operating height on the dynamic performance of this type of vehicle were inspected. Slot thickness to model diameter ratios of 1, 5, and 10% were tested utilizing convergence angles of 0, 30 and 60 degrees.
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1962
- Accession Number
- AD0414393
Entities
People
- Claude A. Foltz
Organizations
- Wichita State University