Studies On Thermal Stresses For Aircraft Structures Exposed To Transient External Heating, Volume II. An Analytical Method For The Prediction Of Behavior Of A Sheet-Stringer Panel With A Uniformly Heated Surface

Item

Title
Studies On Thermal Stresses For Aircraft Structures Exposed To Transient External Heating, Volume II. An Analytical Method For The Prediction Of Behavior Of A Sheet-Stringer Panel With A Uniformly Heated Surface
Date
1955
Index Abstract
Not Available
Photo Quality
Not Needed
Report Number
WADC TR 55-192 Volume 2
Corporate Author
California U.
Laboratory
Aircraft Laboratory
Extent
51
PB Number
PB133924
NTRL Accession Number
AD110408
Identifier
AD0110408
AD0110408
Access Rights
ASTIA
Distribution Classification
1
Contract
AF 33(616)-293
DoD Project
1350
DoD Task
None Given
DTIC Record Exists
No
Distribution Change Authority Correspondence
AFWAL LTR
Distribution Conflict
Fix
Report Availability
Full text available
Date Issued
1955-12
Abstract
The abstract for this report is either unavailable or has yet to be entered
Provenance
Lockheed Martin Missiles & Fire Control
Type
report
Subject
Aerodynamic Heating
Airframes
Thermal Stresses
Sheets
Stresses
Temperature
Format
1 online resource
Creator
Mahlmeister, J. E.