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

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

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