Progress in validation of Wind-US for ramjet/scramjet combustion

W Engblom, F Frate, C Nelson - 43rd AIAA Aerospace Sciences …, 2005 - arc.aiaa.org
There is currently national interest in development of high-speed propulsion systems (eg,
ramjet/scramjet combined cycle) at NASA (eg X-43) and the DoD (eg HyFly). The recent …

Wind-US Users Guide Version 4.0

DA Yoder - 2016 - ntrs.nasa.gov
Wind-US is a computational platform which may be used to numerically solve various sets of
equations governing physical phenomena. Currently, the code supports the solution of the …

Verification, Validation, and Testing of Kinetic Mechanisms of Hydrogen Combustion in Fluid‐Dynamic Computations

VP Zhukov - International Scholarly Research Notices, 2012 - Wiley Online Library
A one‐step, a two‐step, an abridged, a skeletal, and four detailed kinetic schemes of
hydrogen oxidation have been tested. A new skeletal kinetic scheme of hydrogen oxidation …

An Algorithm for Chemically Reacting Flows on Generalized Grids Using a Rule-Based Framework

S Thakur, J Wright, W Shyy - 43rd AIAA Aerospace Sciences Meeting …, 2005 - arc.aiaa.org
Over the last decade significant new technologies have been developed which allow the
scientist/engineer to design reliable programs for simulating the complex physics involved in …

Automated grid independence via unstructured adaptive refinement

R Chila, D Kaminski - 36th AIAA Fluid dynamics conference and exhibit, 2006 - arc.aiaa.org
Grid independence is frequently an overlooked item in CFD analyses. Often an attempt is
made to perform due diligence towards this end, but time and resource constraints prevent …

Reaction ratio and nozzle expansion effects on the PDE

R Dyer, T Kaemming, R Baker - 39th AIAA/ASME/SAE/ASEE Joint …, 2003 - arc.aiaa.org
Two aspects of PDE design and operation are examined using time accurate CFD and
Boeing's PDE cycle deck, DECADE. First, the effect of engine reaction ratio is examined. The …

Verification and Validation of a Homogeneous Reaction Kinetics Model Using a Detailed H2-O2 Reaction Mechanism Versus Chemkin and Cantera

SS Alam, C Depcik - … Engineering Congress and …, 2019 - asmedigitalcollection.asme.org
Increased black-box software use without adequate software literacy can lead to improper
results and potentially disastrous consequences. Furthermore, such software is often …

WIND validation cases: computational study of thermally-perfect gases

T DalBello - 41st Aerospace Sciences Meeting and Exhibit, 2003 - arc.aiaa.org
The ability of the WIND Navier-Stokes code to predict the physics of multi-species gases is
investigated in support of future high-speed, hightemperature propulsion applications …

무격자기법을이용한초음속예혼합조건에대한화학반응수치해석

서지완, 김재승, 서송현, 김규홍 - 한국전산유체공학회지, 2022 - dbpia.co.kr
The scramjet is the supersonic-combustion ramjet engine operating in the hypersonic
regime. Recently, importance of designing regenerative cooling system is highlighted for …

Boundary condition procedures for CFD analyses of propulsion systems-The multi-zone problem

W ROMER, R BUSH - 29th Joint Propulsion Conference and Exhibit, 1993 - arc.aiaa.org
A generic, multi-zone boundary condition procedure has been developed for computational
fluid dynamics (CFD) analyses of propulsion flowfields. The zonal interface scheme …