columbus · Control Surface Oscillatory Coefficients Measured On Low Aspect-Ratio Wings

Control Surface Oscillatory Coefficients Measured On Low Aspect-Ratio Wings

Title: Control Surface Oscillatory Coefficients Measured On Low Aspect-Ratio Wings
Date: 1953
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: WADC TR 53-64
Creator: Beals, V.; Targoff, W. P.
Corporate Author: Cornell Aeronautical Lab Inc Buffalo NY
Extent: 73
NTRL Accession Number: AD026027
Identifier: AD0026027
Distribution Classification: 1
DTIC Record Exists: No
Distribution Change Authority Correspondence: AFFDL LTR
Abstract: Wind tunnel tests were conducted on low aspect ratio wings in order to: (1.) Measure the oscillatory aerodynamic lift forces, pitching moments, and hinge moments acting on rectangular wings of aspect ratio 1 and 2, due to the harmonic vibration of flap or tab; (2.) Measure similar data due to static deflection of flap or tab; (3.) Measure wing pitching moment and flap hinge moment of the finite wings under zero lift conditions; and (4.) Compare these measured data with existing low aspect ratio theory.
Report Availability: Not available via Contrails
Date Issued: 1953-04
Index In: DTIC
Type: report