columbus · Boundary Layer Control Applied To Tail Surfaces Of Aircraft . Part I: Wind Tunnel Report

Boundary Layer Control Applied To Tail Surfaces Of Aircraft . Part I: Wind Tunnel Report

Title: Boundary Layer Control Applied To Tail Surfaces Of Aircraft . Part I: Wind Tunnel Report
Date: 1957
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: WADC TR 57-741 Part 1
Creator: Leisher, L. L.; Gertsen, W. M.
Corporate Author: Cessna Aircraft Company
Laboratory: Flight Control Laboratory
Extent: 159
PB Number: PB137925
Identifier: AD0142216
Access Rights: ASTIA
Distribution Classification: 2
Contract: AF 33(616)-3463
DoD Project: 1365
DoD Task: 13559
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1957-12
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: AFRL/VACA
Type: report