Effects Of Structural Flexibility On Gust Loading Of Aircraft Part II: Dynamic Stresses In Swept-wing Airplanes

Item

Title
Effects Of Structural Flexibility On Gust Loading Of Aircraft Part II: Dynamic Stresses In Swept-wing Airplanes
Date
1954
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
WADC TR 54-592 Part 2
Creator
Kirsch, A. A.
Foss, K. A.
Calligeros, J. M.
Corporate Author
Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory
Aircraft Laboratory
Extent
201
PB Number
PB134845
NTRL Accession Number
AD078081
Identifier
AD0078081
Access Rights
Notice(s)
Distribution Classification
1
Contract
AF 33(616)-2425
DoD Project
None Given
DoD Task
None Given
DTIC Record Exists
No
Distribution Change Authority Correspondence
AFWAL LTR
Distribution Conflict
Fix
Report Availability
Full text available
Date Issued
1955-08
Abstract
The abstract for this report is either unavailable or has yet to be entered
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Format
1 online resource

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