NONLINEAR THERMOELASTIC EFFECTS ON HYPERSONIC STABILITY AND CONTROL. PART III: SIMULATION, MEASUREMENT AND ANALYSIS OF NONLINEAR STATIC AEROTHERMOELASTIC BEHAVIOR OF A 45 DEGREE DELTA WING.
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. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 01, 1965
- Accession Number
- AD0613708
Entities
People
- James R. Batt
Organizations
- Bell Aircraft Corporation