columbus · Aileron Reversal Research of Straight and Swept Wings at High Subsonic Speeds

Aileron Reversal Research of Straight and Swept Wings at High Subsonic Speeds

Title: Aileron Reversal Research of Straight and Swept Wings at High Subsonic Speeds
Date: 1952
Index Abstract: Not Available
Photo Quality: Undetermined
Report Number: WADC TR 52-231
Creator: Goland, L.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Extent: 52
NTRL Accession Number: AD004240
Identifier: AD0004240
AD Number: 4240
Access Rights: Unknown
Distribution Classification: 1
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: AFAL ltr
Distribution Change Action Date: 10/17/2001
Abstract: Wing and aileron aerodynamic characteristics are obtained from experimental data of wings undergoing the phenomenon of aileron reversal. Wind tunnel tests were conducted on both a straight wing and a 45 degree sweptback wing at Mach numbers of 0.6, 0.7, O.8 and O.85. The test results are presented graphically and compared to theoretical and empirical aerodynamic characteristics commonly used in reversal calculations.
Report Availability: Not available via Contrails
Date Issued: 1952-09
Index In: DTIC
Type: report