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

Item

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.