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Perspectives on hypersonic viscous and nonequilibrium flow researchAn attempt is made to reflect on current focuses in certain areas of hypersonic flow research by examining recent works and their issues. Aspects of viscous interaction, flow instability, and nonequilibrium aerothermodynamics pertaining to theoretical interest are focused upon. The field is a diverse one, and many exciting works may have either escaped the writer's notice or been abandoned for the sake of space. Students of hypersonic viscous flow must face the transition problems towards the two opposite ends of the Reynolds or Knudsen number range, which represents two regimes where unresolved fluid/gas dynamic problems abound. Central to the hypersonic flow studies is high-temperature physical gas dynamics; here, a number of issues on modelling the intermolecular potentials and inelastic collisions remain the obstacles to quantitative predictions. Research in combustion and scramjet propulsion will certainly be benefitted by advances in turbulent mixing and new computational fluid dynamics (CFD) strategies on multi-scaled complex reactions. Even for the sake of theoretical development, the lack of pertinent experimental data in the right energy and density ranges is believed to be among the major obstacles to progress in aerothermodynamic research for hypersonic flight. To enable laboratory simulation of nonequilibrium effects anticipated for transatmospheric flight, facilities capable of generating high enthalpy flow at density levels higher than in existing laboratories are needed (Hornung 1988). A new free-piston shock tunnel capable of realizing a test-section stagnation temperature of 10(exp 5) at Reynolds number 50 x 10(exp 6)/cm is being completed and preliminary tests has begun (H. Hornung et al. 1992). Another laboratory study worthy of note as well as theoretical support is the nonequilibrium flow experiment of iodine vapor which has low activation energies for vibrational excitation and dissociation, and can be studied in a laboratory with modest resources (Pham-Van-Diep et al. 1992).
Document ID
19920024169
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cheng, H. K.
(University of Southern California Los Angeles, CA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Aerodynamics
Report/Patent Number
USCAE-151
NAS 1.26:190817
NASA-CR-190817
Report Number: USCAE-151
Report Number: NAS 1.26:190817
Report Number: NASA-CR-190817
Accession Number
92N33413
Funding Number(s)
CONTRACT_GRANT: NAGW-1061
CONTRACT_GRANT: AF-AFOSR-0104-91
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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