columbus · Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume I, Aerodynamics

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume I, Aerodynamics

Title: Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume I, Aerodynamics
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: FDL TDR 64-16 Part 1 Volume 1
Corporate Author: Bell Aerosystems Company
Extent: 82
Identifier: AD0608469
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: Linnell's 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.
Report Availability: Full text available
Date Issued: 1964-09
Laboratory: AF Flight Dynamics Laboratory
Provenance: Lockheed Martin Missiles & Fire Control; AFRL/VACA
Type: report
Format: 1 online resource
Creator: Batt, James R.