columbus · A Preliminary Design Analysis of a Multi-Channel Ejector Thrust Augmentation Concept with Oval or Rectangular Air Supply Ducts

A Preliminary Design Analysis of a Multi-Channel Ejector Thrust Augmentation Concept with Oval or Rectangular Air Supply Ducts

Title: A Preliminary Design Analysis of a Multi-Channel Ejector Thrust Augmentation Concept with Oval or Rectangular Air Supply Ducts
Index Abstract: Not Available
Photo Quality: Not Needed
Report Number: ARL 72-0062
Index Price: $0.00
Report Availability: Full text available
Creator: Wright, D. C.; Allen, J. G.; Meholick, W. N.; Salter, G. R.; Ashby, R.; Tilyou, C.
Date: 1972
Extent: 77
Corporate Author: Bell Aerospace Company
Laboratory: Aerospace Research Laboratories
Identifier: AD0744839; AD0744839
Contract: F33615-71-C-1802
DoD Project: 7116
Distribution Conflict: No
Access Rights: Approved for public release; distribution unlimited.
Distribution Classification: 1
Date Issued: 1972-05
Abstract: The abstract for this report is either unavailable or has yet to be entered
Date Modified: Scanned by request 7/1/2020 submitted by a private citizen (Private Citizen)
DTIC Record Exists: Yes
Provenance: Bombardier/Aero
Type: report
Format: 1 online resource (xii, 59 pages) : ill.
Subject: Short Takeoff Aircraft; Nozzle Area Ratio; Thrust Augmentation; Duct Inlets; Shear Stresses; Buckling; Sandwich Construction; Compressive Properties; Exhaust Diffusers; Configurations
AD Number: AD 744839
NTRL Accession Number: AD744839