Amanote Research

Amanote Research

    RegisterSign In

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

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

Available in full text

Categories
Aerospace Engineering
Date

September 1, 1999

Authors
Farooq SaeedMichael S. SeligMichael B. Bragg
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

© 2025 Amaplex Software S.P.R.L. All rights reserved.

Privacy PolicyRefund Policy