Author: Atherton A. Carty
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 116
Book Description
Data are acquired in a simple coannular He/air supersonic jet suitable for validation of CFD codes for high speed propulsion. Helium is employed as a non-reacting hydrogen fuel simulant, constituting the core of the coannular flow while the coflow is composed of air. The mixing layer interface between the two flows in the near field and the plume region which develops further downstream constitute the primary regions of interest, similar to those present in all hypersonic air breathing propulsion systems. A computational code has been implemented from the experiment's inception, serving as a tool for model design during the development phase.
Development and Validation of a Supersonic Helium-Air Coannular Jet Facility
Author: Atherton A. Carty
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 116
Book Description
Data are acquired in a simple coannular He/air supersonic jet suitable for validation of CFD codes for high speed propulsion. Helium is employed as a non-reacting hydrogen fuel simulant, constituting the core of the coannular flow while the coflow is composed of air. The mixing layer interface between the two flows in the near field and the plume region which develops further downstream constitute the primary regions of interest, similar to those present in all hypersonic air breathing propulsion systems. A computational code has been implemented from the experiment's inception, serving as a tool for model design during the development phase.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 116
Book Description
Data are acquired in a simple coannular He/air supersonic jet suitable for validation of CFD codes for high speed propulsion. Helium is employed as a non-reacting hydrogen fuel simulant, constituting the core of the coannular flow while the coflow is composed of air. The mixing layer interface between the two flows in the near field and the plume region which develops further downstream constitute the primary regions of interest, similar to those present in all hypersonic air breathing propulsion systems. A computational code has been implemented from the experiment's inception, serving as a tool for model design during the development phase.
Aeroacoustics of Flight Vehicles
Author: Harvey H. Hubbard
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 620
Book Description
Publisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 620
Book Description
NASA Technical Memorandum
Scientific and Technical Aerospace Reports
29th AIAA Fluid Dynamics Conference
Large-Eddy Simulations of Turbulence
Author: M. Lesieur
Publisher: Cambridge University Press
ISBN: 9780521781244
Category : Mathematics
Languages : en
Pages : 240
Book Description
Large-Eddy Simulations of Turbulence is a reference for LES, direct numerical simulation and Reynolds-averaged Navier-Stokes simulation.
Publisher: Cambridge University Press
ISBN: 9780521781244
Category : Mathematics
Languages : en
Pages : 240
Book Description
Large-Eddy Simulations of Turbulence is a reference for LES, direct numerical simulation and Reynolds-averaged Navier-Stokes simulation.