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Measurement of Angular Displacements of Practical Wing Structures by the Moire' Fringe Technique

Title: Measurement of Angular Displacements of Practical Wing Structures by the Moire' Fringe Technique
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: FDL TDR 64-42
Creator: Padlog, Joseph; Gallagher, Richard H.
Corporate Author: Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Extent: 56
Identifier: AD0608470
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(657)-7486
DoD Project: 8219
DoD Task: 821901
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: Results of a study of the feasibility of employing the Moire' fringe technique in the measurement of angular displacements of practical wing structures are presented. Slope influence coefficients obtained from Moire' fringe patterns determined from a square cantilever plate and a swept wing model are compared with available theoretical and experimental data.
Report Availability: Full text available
Date Issued: 1964-09
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource