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

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

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Matrix Methods in Structural Mechanics