columbus · Aerodynamic Heating Simulation: Part I. Theory and Program Definition

Aerodynamic Heating Simulation: Part I. Theory and Program Definition

Title: Aerodynamic Heating Simulation: Part I. Theory and Program Definition
Date: 1964
Index Abstract: Coming Soon
Photo Quality: Complete
Report Number: FDL TDR 64-112 Part 1
Creator: Crump, Glendon R.
Corporate Author: Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Extent: 42
Identifier: AD0608070
Access Rights: Notice(s)
Distribution Classification: 1
Contract: Laboratory Research - No Contract
DoD Project: 1347
DoD Task: 134703
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Abstract: The study was conducted to determine how accurately aerodynamic heating is simulated in the laboratory with radiant heat lamps under computer control. A study of aerodynamic heating theory resulted in the preparation of a digital computer program for calculating the parameters required as input data for the heat rate computer. The heat rate computer is used to control the heat input to an actual flight test specimen. Laboratory test results are compared with flight measured data to determine the degree of simulation. Test results indicate that aerodynamic heating may be adequately simulated up to 600F. Laboratory simulation to higher temperatures is being studied for future programs.
Report Availability: Full text available
Date Issued: 1964-09
Provenance: Lockheed Martin Missiles & Fire Control
Type: report
Format: 1 online resource