Perspectives on Hypersonic Viscous and Nonequilibrium Flow Research

Released on by National Aeronaut Administration (Nasa)
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  • Perspectives on Hypersonic Viscous and Nonequilibrium Flow Research Book Detail

  • Author : National Aeronaut Administration (Nasa)
  • Release Date : 2018-07-10
  • Publisher : Createspace Independent Publishing Platform
  • Genre :
  • Pages : 54
  • ISBN 13 : 9781722689681
  • File Size : 16,16 MB
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Perspectives on Hypersonic Viscous and Nonequilibrium Flow Research by National Aeronaut Administration (Nasa) PDF Summary

Book Description: An 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 resou...

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Theoretical and Applied Aerodynamics

Theoretical and Applied Aerodynamics

File Size : 9,9 MB
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This book covers classical and modern aerodynamics, theories and related numerical methods, for senior and first-year graduate engineering students, including: