Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part II, Analytical and Experimental Statis Aerothermoelasticity

Item

Title
Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part II, Analytical and Experimental Statis Aerothermoelasticity
Date
1964
Index Abstract
Coming Soon
Photo Quality
Not Needed
Report Number
FDL TDR 64-16 Part 2
Creator
Batt, James R.
Gallagher, Richard H.
Corporate Author
Bell Aerosystems Company
Extent
92
Identifier
AD0608476
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(657)-7486
DoD Project
8219
DoD Task
821901
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
An analytical method was developed for the analysis of static aerothermoelastic behavior in the presence of nonlinear aerodynamic loads and geometrically nonlinear structural behavior. The method was programmed for the IBM 7090 digital computer using FORTRAN coding techniques. A system for the experimental determination of static aerothermoelastic response of nonuniformly heated structures to loadings which are a nonlinear function of wing surface slopes was developed. Results of this experimental program are presented and compared with theoretical predictions.
Report Availability
Full text available
Date Issued
1964-10
Laboratory
AF Flight Dynamics Laboratory
Provenance
Lockheed Martin Missiles & Fire Control
AFRL/VACA
Type
report
Format
1 online resource