Experimental Investigation of Temperature and Velocity Distribution About a Rocket Jet
Author: Whitmore, Quentin Robert
Year: 1947
Degree: Master's thesis
Advisor: Unknown, Unknown
Committee Member: Unknown, Unknown
Option: Aeronautics; Electrical Engineering
DOI: 10.7907/SN1E-KS25
Abstract
The purpose of the investigation was to determine the temperature distribution and velocity profile surrounding the wake of a 1500 pound thrust liquid rocket motor. The temperature measurements were restricted to those 500°F and below. The velocities measured were in the region in which the temperature measurements were made.
The region in which the temperatures exceeded 500°F was found to be included within a solid angle of ten degrees. The high temperature region was found to be larger than the high velocity region.
The investigation was carried out during the academic year 1946-1947 at GALCIT Jet Propulsion Laboratory under the supervision of Dr. Robert H. Boden.
Files
- Whitmore_qr_1947.pdf (application/pdf)