columbus · Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure: Supplement I - Dynamic Modeling of Complex Structures

Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure: Supplement I - Dynamic Modeling of Complex Structures

Title: Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure: Supplement I - Dynamic Modeling of Complex Structures
Index Abstract: Not Available
Photo Quality: Incomplete
Report Number: ASD TDR 62-801 Supplement I
Index Price: $0.00
Report Availability: Full text available by request
Creator: Roberts, W. H.; Finwall, P. E.
Date: 1964
Extent: 249
Laboratory: AF Flight Dynamics Laboratory
Identifier: AD0600234
Corporate Report Number: NOR 63-139
Contract: AF 33(657)-10075
DoD Project: 1370
DoD Task: 137005
Distribution Conflict: No
Access Rights: OTS
Distribution Classification: 1
Special Scanning Requirements: Foldout pages
Date Issued: 1964-04
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bombardier/Aero
Type: report