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Combustion of LOX with H2(sub g) under subcritical, critical, and supercritical conditions (Task 1) and experimental observation of dense spray and mixing of impinging jets (Task 2)
Document ID: 19920010833
NTRS Full-Text: Click to View  [PDF Size: 6.1 MB]
Author: Kuo, K. K.; Hsieh, W. H.; Cheung, F. B.; Yang, A. S.; Brown, J. J.; Woodward, R. D.; Kline, M. C.; Burch, R. L.
Abstract: The objective was to achieve a better understanding of the combustion processes of liquid oxygen and hide
Publication Year: 1992
Document Type: Technical Report
Report/Patent Number: NASA-CR-190113, NAS 1.26:190113
Date Acquired: Nov 07, 1995
A study of NACA and NASA published information of pertinence in the design of light aircraft. Volume 2 - Aerodynamics and aerodynamic loads
Document ID: 19700012724
NTRS Full-Text: Click to View  [PDF Size: 32.6 MB]
Author: Perkins, J. N.; Summey, D. C.; Williams, J. C., III
Abstract: Critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load hide
Publication Year: 1970
Document Type: Technical Report
Report/Patent Number: NASA-CR-1485
Date Acquired: Nov 22, 1995
Injection Principles from Combustion Studies in a 200-Pound-Thrust Rocket Engine Using Liquid Oxygen and Heptane
Document ID: 20050019330
NTRS Full-Text: Click to View  [PDF Size: 21.2 MB]
Author: Heidmann, M. F.; Auble, C. M.
Abstract: The importance of atomizing and mixing liquid oxygen and heptane was studied in a 200-pound-thrust hide
Publication Year: 1955
Document Type: Technical Report
Report/Patent Number: NACA-RM-E55C22, L-3572
Date Acquired: Jan 12, 2005
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