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

Download this report (PDF, 11.01 MB, 56 pages)
Report Number: FDL TDR 64-42
Author(s): Padlog, Joseph, Gallagher, Richard H.
Corporate Author(s): Bell Aerosystems Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Pages: 56
Contract: AF 33(657)-7486
DoD Project: 8219
DoD Task: 821901
Identifier: AD0608470

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.

Provenance: Lockheed Martin Missiles & Fire Control

Other options for obtaining this report:

Via the Defense Technical Information Center (DTIC):
A record for this report, and possibly a pdf download of the report, exists at DTIC

Via National Technical Report Library:
This report may be available for download from NTRL. Use the Title from this record to locate the item in DTIC Online

Indications of Public Availability
No digital image of an index entry indicating public availability is currently available
The inside cover of this report indicates that it was released for public sale