Accession Number:

AD0608469

Title:

NONLINEAR THERMOELASTIC EFFECTS ON HYPERSONIC STABILITY AND CONTROL, PART I, VOLUME I, AERODYNAMICS,

Descriptive Note:

Corporate Author:

BELL AEROSYSTEMS CO BUFFALO N Y

Personal Author(s):

• Batt,James R.

Report Date:

1964-09-01

Pagination or Media Count:

72.0

Abstract:

Linnells pressure prediction method is used as a basis for developing hypersonic aerodynamic influence coefficient matrices. The method developed accounts for the nonlinear variation of lifting pressure with angle of attack which is present at hypersonic speeds. Comparisons of theoretical and experimental hypersonic pressure distributions are made. Author

Descriptors:

• (*HYPERSONIC FLIGHT
• AERODYNAMIC CHARACTERISTICS)
• (*AERODYNAMIC CHARACTERISTICS
• HYPERSONIC FLIGHT)
• (*AEROTHERMOELASTICITY
• FLUID DYNAMICS)
• AIRFOILS
• LIFT
• NONLINEAR SYSTEMS
• STABILITY
• CONTROL
• PRESSURE
• MATHEMATICAL ANALYSIS
• MATRICES(MATHEMATICS)
• ANGLE OF ATTACK
• WINGS

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE