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Development of High Temperature Flutter Transducer

Title: Development of High Temperature Flutter Transducer
Date: 1965
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: AFFDL TR 65-21
Creator: Day, David L.
Corporate Author: Allegany Instrument Company
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 99
NTRL Accession Number: AD465262
Identifier: AD0465262
Access Rights: Notice(s)
Distribution Classification: 1
Contract: AF 33(615-1793
DoD Project: 1469
DoD Task: 146907
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFFDL LTR
Special Scanning Requirements: fold out pages
Abstract: The design, development, and testing of two hightemperature transducers are described. One measures vibration amplitude and frequency, and the other measures acceleration. Both were designed to detect aerodynamic panel flutter during boost and re-entry of the X-20 Dynasoar, then under development. These transducers are electrical resistance strain gage types. Part details discussed are the pendulum, damper, sealing, and case configuration. Both transducers are also discussed in greater detail with respect to natural frequency, damping, strain gage application, and output.
Report Availability: Full text available
Date Issued: 1965-03
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource