columbus · Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume 2, Aerodynamics

Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume 2, Aerodynamics

Title: Nonlinear Thermoelastic Effects on Hypersonic Stability and Control: Part I, Volume 2, Aerodynamics
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: FDL TDR 64-16 Part 1 Volume 2
Corporate Author: Bell Aerosystems Company
Extent: 142
Identifier: AD0608829
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: The curves presented in this volume of the final report are to be used to obtain aerodynamic influence coefficient matrices for slender two-dimensional airfoils in hypersonic inviscid flow. Influence coefficients are presented for ten airfoil shapes as a function of thickness ratio, Mach number and geometric angle of attack.
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.