Hybrid Airfoil Design Procedure Validation for Full-Scale Ice Accretion Simulation

Journal of Aircraft - United States
doi 10.2514/2.2532
Full Text
Abstract

Available in full text

Date
Authors
Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Related search

A Hybrid Airfoil Design Method for Icing Wind Tunnel Tests

2013English

Numerical Analysis of Ice Accretion Effects at Super-Cooled Large Droplet Conditions on Airfoil Aerodynamics

Journal of Modern Transportation
Electronic EngineeringComputer Science ApplicationsElectricalMechanical EngineeringTransportation
2011English

Ice Accretion on Aircraft

Nature
Multidisciplinary
1935English

Numerical Simulation of Airfoil Thermal Anti-Ice Operation, Part 2:Implementation and Results

Journal of Aircraft
Aerospace Engineering
2007English

New Numerical Simulation Procedure for Large-Scale Debris Flows (Kanako-Ls)

International Journal of Erosion Control Engineering
2013English

An Inverse Approach for Airfoil Design

2008English

Ice Accretion and Icing Technology

2015English

Development of Simulation Codes for ATES. 1st Report. Full-Scale Code.

Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Condensed Matter PhysicsMechanical Engineering
1993English

A Study of Scaling for Intercycle Ice Accretion Tests

2001English

Amanote Research

Note-taking for researchers

Follow Amanote

© 2024 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy