Investigation of Feasible Nozzle Configurations for Noise Reduction in Turbofan and Turbojet Aircraft. Volume II. Slot Nozzle Configuration.
Abstract
This volume contains a description of results obtained for two dimensional rectangular slot nozzles without and with straight attached flaps. Three appendices are included in this volume containing results of other research activities.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jul 01, 1975
- Accession Number
- ADA024959
Entities
People
- B. H. Goethert
- Grant T. Patterson
- J. R. Maus
- Mahendra C. Joshi
- William A. Dunhill
Organizations
- University of Tennessee Space Institute