Computational methodology for bleed air ice protection system parametric analysis

R Domingos, M Papadakis, A Zamora - AIAA Atmospheric and Space …, 2010 - arc.aiaa.org
I. Introduction nti-icing systems use thermal energy from electrical or hot-air sources to
reduce or eliminate ice accretion on critical aerodynamic surfaces. In most aircraft using …

Proposed wall function models for heat transfer around a cylinder with rough surface in cross flow

GAL da Silva, MN Arima, NN Branco… - 2011 - sae.org
This paper proposes wall function models to simulate the heat transfer around a cylinder in
cross flow with an isothermal and rough surface. The selected case has similitudes with …

Assessment of the state of the art of integrated vehicle health management technologies as applicable to damage conditions

MS Reveley, T Kurtoglu, KM Leone, JL Briggs… - 2010 - ntrs.nasa.gov
A survey of literature from academia, industry, and other Government agencies assessed the
state of the art in current integrated vehicle health management (IVHM) aircraft technologies …

Numerical Simulation of In-Flight Icing via a Particle-Based Morphogenetic Method

K Szilder, EP Lozowski - Handbook of Numerical Simulation of In-Flight …, 2023 - Springer
Most current numerical ice accretion models are constrained by their reliance on solving
continuous partial differential equations for energy, momentum, and mass conservation. This …

Numerical Simulation of Coupled Heat and Mass Transfer for Airfoil Ice Protection Systems

G Araujo Lima da Silva, DR de Barros… - Handbook of Numerical …, 2023 - Springer
The design of ice thermal protection systems is multidisciplinary and highly integrated with
that of other aircraft systems and aircraft aerodynamics, thus requiring knowledge of …

[PDF][PDF] Numerical Simulation of Convective Heat Transfer for In-Flight Icing

GAL da Silva, DR de Barros, DM Pio, CF Rafael… - 2023 - aerothermalsolutions.co
Convective heat transfer is the primary mechanism during glaze ice accretion. Hence,
modeling heat transfer over rough surfaces and the laminar-turbulent transition is essential …

Sensitivity analysis of a bleed air anti-ice thermal model to geometrical and operational parameters

L Santos, R Domingos, R Maria, M Leal - 46th AIAA Aerospace …, 2008 - arc.aiaa.org
The are several different phenomena involved in the simulation of an anti-ice protection
system coupled with several geometrical and operational parameters which define actual …

Numerical Simulation of Convective Heat Transfer for In-Flight Icing

G Araujo Lima da Silva, DR de Barros, DM Pio… - Handbook of Numerical …, 2023 - Springer
Convective heat transfer is the primary mechanism during glaze ice accretion. Hence,
modeling heat transfer over rough surfaces and the laminar-turbulent transition is essential …

Assessment of the State of the Art of Flight Control Technologies as Applicable to Adverse Conditions

M Reveley, JL Briggs, KM Leone, T Kurtoglu… - 2010 - trid.trb.org
Literature from academia, industry, and other Government agencies was surveyed to assess
the state of the art in current Integrated Resilient Aircraft Control (IRAC) aircraft technologies …

Assessment of the State of the Art of Flight Control Technologies as Applicable to Adverse Conditions

JL Briggs, KM Leone, T Kurtoglu, CA Withrow - 2010 - ntrs.nasa.gov
Literature from academia, industry, and other Government agencies was surveyed to assess
the state of the art in current Integrated Resilient Aircraft Control (IRAC) aircraft technologies …