Accession Number : ADP000232
Title : An Application of the Molecular Beam Time-of-Flight Technique to Measurements of Thermal Boundary Layer Effects on Mass Sampling from a Shock Tube,
Corporate Author : KYOTO UNIV (JAPAN) DEPT OF AERONAUTICAL ENGINEERING
Personal Author(s) : Teshima,K. ; Takahashi,N. ; Deguchi,M.
Report Date : JUL 1981
Pagination or Media Count : 8
Abstract : A shock heated molecular beam (SHMB) is useful for study of the molecular reaction dynamics especially those including internally excited molecules. A time-of-flight (TOF) method to analyze the velocity distribution of the beam molecules can be used to determine their internal states by using the energy conservation and has been used for the conventional molecular beams.
Descriptors : *Molecular beams, *Boundary layer, *Shock tubes, *Shock waves, *Heating, *Reaction kinetics, Japan
Distribution Statement : APPROVED FOR PUBLIC RELEASE