columbus · Study To Determine An Automatic Flight Control Configuration To Provide A Stability Augmentation Capability For High Performance Supersonic Aircraft

Study To Determine An Automatic Flight Control Configuration To Provide A Stability Augmentation Capability For High Performance Supersonic Aircraft

Title: Study To Determine An Automatic Flight Control Configuration To Provide A Stability Augmentation Capability For High Performance Supersonic Aircraft
Date: 1957
Index Abstract: Limited
Photo Quality: Incomplete
Report Number: WADC TR 57-349
Creator: Van Meter, J. T.; McLane, R. C.
Corporate Author: Minneapolis-Honeywell Regulator Company
Extent: 60
PB Number: PB140957
Identifier: AD0206591
Access Rights: Notice(s)
Distribution Classification: 2
Contract: AF 33(616)-5039
DoD Project: 5106
DoD Task: 82033
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1957-06
Abstract: The abstract for this report is either unavailable or has yet to be entered
Laboratory: Flight Control Laboratory
Provenance: AFRL/VACA
Type: report