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

Item

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