columbus · Theoretical Investigation of the Longitudinal Response Characteristics of a Swept-Wing Fighter Airplane Having a Pitch-Attitude Control System

Theoretical Investigation of the Longitudinal Response Characteristics of a Swept-Wing Fighter Airplane Having a Pitch-Attitude Control System

Title: Theoretical Investigation of the Longitudinal Response Characteristics of a Swept-Wing Fighter Airplane Having a Pitch-Attitude Control System
Date: 1953
Index Abstract: Limited
Photo Quality: Undetermined
Report Number: NACA TN 2882
Creator: Stokes, Fred H.; Matthews, J. T.
Corporate Author: Langley Aeronautical Laboratory
Laboratory: Langley Aeronautical Laboratory
Extent: 45
PB Number: PB108606
Identifier: AD0001470
Access Rights: Unknown
Distribution Classification: 2
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1953-01
Abstract: The abstract for this report is either unavailable or has yet to be entered
Index In: PB/AD Index
Type: report