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Author
Richmond, J. K. | Shreeve, R. P.
Title
New Techniques for Obtaining Kinetic Data With Shock-Induced Combustion.
Coporate
Boeing Scientific Research Labs., Seattle, WA
Report
AIAA Paper 67-105,
Book or Conf
American Institute of Aeronautics and Astronautics (AIAA). Aerospace Sciences Meeting, 5th. AIAA Paper 67-105. January 23-26, 1967, New York, New York, 1-12 p., 1967
Keywords
kinetics | combustion | fuel/air mixtures | wind tunnels | contamination | shock tubes | fuel injection | velocity | pressure
Identifiers
induction time