columbus · Flutter Tests of Large Straight Wing Models at High Subsonic Speeds

Flutter Tests of Large Straight Wing Models at High Subsonic Speeds

Title: Flutter Tests of Large Straight Wing Models at High Subsonic Speeds
Date: 1955
Index Abstract: Not Available
Photo Quality: Complete
Report Number: WADC TR 55-334
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Extent: 150
NTRL Accession Number: AD110555
Identifier: AD0110555
Access Rights: ASTIA
Distribution Classification: 1
Contract: AF 33(038)-9734
DoD Project: 1370
DoD Task: 13473
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Report Availability: Full text available
Date Issued: 1955-12
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource
Creator: White, Richard P., Jr.