columbus · Charts of Sphere Stagnation Heat-Transfer Rate in Air and Nitrogen at High Temperatures

Charts of Sphere Stagnation Heat-Transfer Rate in Air and Nitrogen at High Temperatures

Title: Charts of Sphere Stagnation Heat-Transfer Rate in Air and Nitrogen at High Temperatures
Date: 1963
Index Abstract: Coming Soon
Photo Quality: Not Needed
Report Number: AEDC TDR 63-139
Corporate Author: ARO, Inc.
Extent: 17
Identifier: AD0409870
Distribution Classification: 1
Contract: AF 40(600)-1000
DoD Project: None Given
DoD Task: None Given
DTIC Record Exists: Yes
Distribution Change Authority Correspondence: None
Abstract: Fay and Riddell's theory for laminar heat trans fer at the stagnation point is applied to the sphere in equilibrium air and nitrogen. Charts are presented of the heat-transfer rate as a function of stagnation temperature and pressure or free-stream velocity and stagnation pressure in the pressure range between 0.1 and 10 A. and in the temperature range from 2000 to 15,000 K. The effects of Lewis number are considered. Com parisons between Fay and Riddell's theory, the recent theory of Fay and Kemp, and Shock-tube experiments are presented.
Report Availability: Full text available by request
Date Issued: 1963-07
Publisher: Arnold Air Force Station, TN : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force
Provenance: IIT
Type: report
Format: 17 pages ; 28 cm.
Creator: Lewis, Clark H.