columbus · Thermo-elastic Stress due to Aerodynamic Heating of Supersonic Wings. Part 3. Experimental Investigation of the Distribution of Temperature and Thermal Stresses and Deflections

Thermo-elastic Stress due to Aerodynamic Heating of Supersonic Wings. Part 3. Experimental Investigation of the Distribution of Temperature and Thermal Stresses and Deflections

Title: Thermo-elastic Stress due to Aerodynamic Heating of Supersonic Wings. Part 3. Experimental Investigation of the Distribution of Temperature and Thermal Stresses and Deflections
Date: 1953
Index Abstract: Online
Photo Quality: Undetermined
Report Number: AF TR 6351 Part 3
Creator: Loving, D. L.; Stephenson, F. A.
Corporate Author: Colorado Engineering Experiment Station
Extent: 213
PB Number: PB118985
Identifier: AD0027725
Access Rights: Unknown
Distribution Classification: 2
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Index Price: $9.60
Report Availability: Not available via Contrails
Date Issued: 1953-08
Abstract: The abstract for this report is either unavailable or has yet to be entered
Index In: U.S. Government Research Reports
Type: report

Media: http://contrails.iit.edu/DigitalCollection/abstracts/images/PB118985.gif