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

Item

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