columbus · Wind Tunnel Tests Of Shrouded Propellers At Mach Numbers From 0 To 0.60

Wind Tunnel Tests Of Shrouded Propellers At Mach Numbers From 0 To 0.60

Title: Wind Tunnel Tests Of Shrouded Propellers At Mach Numbers From 0 To 0.60
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: WADC TR 58-604
Creator: Grose, Ronald M.
Extent: 207
Access Rights: Unknown
DTIC Record Exists: No
Report Availability: Not available via Contrails
Abstract: The abstract for this report is either unavailable or has yet to be entered
Index In: U.S. Government Research Reports
Type: report
Date: 1958
Date Issued: 1958-12
Corporate Author: United Aircraft Research Laboratories
NTRL Accession Number: PB154504
Identifier: AD0205464