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Stagnation Point Heat Transfer in High Enthalpy Gas Flows, Part I: Convective Heat Transfer in Partially Ionized Air

Title: Stagnation Point Heat Transfer in High Enthalpy Gas Flows, Part I: Convective Heat Transfer in Partially Ionized Air
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: FDL TDR 64-41 Part 1
Creator: Nerem, Robert M.; Stickford, George H.
Corporate Author: Ohio State University
Laboratory: Flight Dynamics Laboratory
Extent: 48
Identifier: AD0601370
Access Rights: OTS
Distribution Classification: 1
Contract: AF 33(657)-10110
DoD Project: 1366
DoD Task: 136615
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: Using an arc driven shock tube facility, measurements of convective heat transfer at the stagnation point of a blunt body were carried out at simulated flight velocities ranging from 20,000 to 40,000 feet per second. These measurements were performed using standard calorimeter techniques with air as the test media. The results indicate no significant ionization effects on aerodynamic heating and indicate that the Lee's approximate equation for stagnation point heat transfer can be used for engineering calculations at flight velocities up to 40,000 feet per second.
Report Availability: Full text available
Date Issued: 1964-03
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource