columbus · 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

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

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