Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part III: Heat Transfer Data for Delta Wing Surface

Item

Title
Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part III: Heat Transfer Data for Delta Wing Surface
Date
1964
Index Abstract
Coming Soon
Photo Quality
Complete
Report Number
FDL TDR 64-2 Part 3
Corporate Author
Grumman Aircraft Engineerign Corporation
Laboratory
Air Force Flight Dynamics Laboratory
Extent
128
Identifier
AD0601804
Access Rights
OTS
Distribution Classification
1
Contract
AF 33(616)-8130
DoD Project
8219
DoD Task
821902
DTIC Record Exists
No
Distribution Change Authority Correspondence
None
Abstract
The report presents heat transfer data obtained in the AEDC 50-inch Mach 8 tunnel on the lower surface of a blunt pyramidal configuration having remotely controlled trailing edge flaps.
Report Availability
Full text available
Date Issued
1964-05
Provenance
AFRL/VACA
Type
report
Format
1 online resource
Creator
Kaufman, Louis G., II