columbus · Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing

Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing

Title: Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing
Date: 1965
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: FDL TDR 64-16 Part 3
Corporate Author: Bell Aerosystems Co.
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 58
Identifier: AD0613708
Access Rights: Notice(s)
Distribution Classification: 1
Contract: AF 33(657)-7486
DoD Project: 8219
DoD Task: 821901
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: Results are presented of additional nonlinear structuralaerodynamic interaction experiments and analyses conducted on a 45 degree delta wing. The aeroelastic simulation scheme developed and described in AD-608 476 was used to experimentally determine the static aerothermoelastic behavior of the subject model wing. Test data were compared with theoretical predictions using a digital computer program.
Report Availability: Full text available
Date Issued: 1965-02
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource
Creator: Batt, James R.