Accession Number:

AD0613708

Title:

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.

Descriptive Note:

Final rept.

Corporate Author:

BELL AEROSYSTEMS CO BUFFALO N Y

Personal Author(s):

• BATT,James R.

Report Date:

1965-02-01

Pagination or Media Count:

57.0

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

Descriptors:

• *DELTA WINGS
• HYPERSONIC FLOW
• AEROTHERMOELASTICITY
• AERODYNAMIC LOADING
• AERODYNAMIC HEATING
• AEROSTATICS
• LIFT
• STABILITY
• CONTROL
• MODEL TESTS
• SIMULATION
• ITERATIONS
• MEASUREMENT
• COMPUTER PROGRAMMING

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE