Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure

Item

Title
Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure
Date
1963
Index Abstract
Not Available
Photo Quality
Undetermined
Report Number
ASD TDR 62-801
Creator
Roberts, W. H.
Finwall, P. E.
White, R. W.
Eldred, K. E.
Corporate Author
Northup Corporation
Laboratory
Flight Dynamics Laboratory
Extent
337
Identifier
AD0600234
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(616)-8219
DoD Project
1370
DoD Task
137009
DTIC Record Exists
Yes
Distribution Change Authority Correspondence
None
Distribution Conflict
No
Report Availability
Full text available
Date Issued
1963-08
Abstract
The abstract for this report is either unavailable or has yet to be entered
Provenance
Jim Kinney
Type
report
Format
1 online resource