Improved Linear Axisymetric Shell-Fluid Model for Launch Vehicle Longitudinal Response Analysis

Item

Title
Improved Linear Axisymetric Shell-Fluid Model for Launch Vehicle Longitudinal Response Analysis
Date
1966
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
AFFDL-TR-66-80 p. 823-847
Creator
Archer, J. S.
Rubin, C. P.
Corporate Author
TRW Systems
Laboratory
Air Force Flight Dynamics Laboratory
Extent
25
Access Rights
Distribution of this document is unlimited.
Distribution Classification
1
Contract
Laboratory Research - No Contract
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Report Availability
Full text available
Date Issued
1966-11
Abstract
The abstract for this report is either unavailable or has yet to be entered
Identifier
AD0646300
Provenance
Bombardier/Aero
Type
article
Format
1 online resource
Is Part Of
Matrix Methods in Structural Mechanics
Media
AFFDLTR66-080article30.pdf

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Items with "Has Part: Improved Linear Axisymetric Shell-Fluid Model for Launch Vehicle Longitudinal Response Analysis"
Title Class
Matrix Methods in Structural Mechanics