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Analytical Ice Shape Predictions for Flight in Natural Icing Conditions

Analytical Ice Shape Predictions for Flight in Natural Icing Conditions PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Book Description


Analytical Ice Shape Predictions for Flight in Natural Icing Conditions

Analytical Ice Shape Predictions for Flight in Natural Icing Conditions PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

Book Description


Analytical Ice Shape Predictions for Flight in Natural Icing Conditions

Analytical Ice Shape Predictions for Flight in Natural Icing Conditions PDF Author: Brian M. Berkowitz
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 0

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 308

Book Description


Ice Accretion and Icing Technology

Ice Accretion and Icing Technology PDF Author: Robert J Flemming
Publisher: SAE International
ISBN: 0768081890
Category : Technology & Engineering
Languages : en
Pages : 122

Book Description
The effects of inflight atmospheric icing can be devastating to aircraft. Universities and industry have been hard at work to respond to the challenge of maintaining flight safety in all weather conditions. Proposed changes in the regulations for operation in icing conditions are sure to keep this type of research and development at its highest level. This is especially true for the effects of ice crystals in the atmosphere, and for the threat associated with supercooled large drop (SLD) icing. This collection of ten SAE International technical papers brings together vital contributions to the subject. Icing on aircraft surfaces would not be a problem if a material were discovered that prevented the freezing and accretion of supercooled drops. Many options that appeared to have promising icephobic properties have had serious shortfalls in durability. This title addresses, among other topics, the measurement techniques and the drop physics that apply to icing, certification for flight through ice crystal clouds and in supercooled large drops, improvements in predictive techniques, scaling methods, test facilities and techniques, and rotorcraft icing.

Aircraft Ice Protection

Aircraft Ice Protection PDF Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 60

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1042

Book Description


Dra/Nasa/Onera Collaboration on Icing Research. Part 2; Prediction of Airfoil Ice Accretion

Dra/Nasa/Onera Collaboration on Icing Research. Part 2; Prediction of Airfoil Ice Accretion PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781729330555
Category : Science
Languages : en
Pages : 56

Book Description
This report presents results from a joint study by DRA, NASA, and ONERA for the purpose of comparing, improving, and validating the aircraft icing computer codes developed by each agency. These codes are of three kinds: (1) water droplet trajectory prediction, (2) ice accretion modeling, and (3) transient electrothermal deicer analysis. In this joint study, the agencies compared their code predictions with each other and with experimental results. These comparison exercises were published in three technical reports, each with joint authorship. DRA published and had first authorship of Part 1 - Droplet Trajectory Calculations, NASA of Part 2 - Ice Accretion Prediction, and ONERA of Part 3 - Electrothermal Deicer Analysis. The results cover work done during the period from August 1986 to late 1991. As a result, all of the information in this report is dated. Where necessary, current information is provided to show the direction of current research. In this present report on ice accretion, each agency predicted ice shapes on two dimensional airfoils under icing conditions for which experimental ice shapes were available. In general, all three codes did a reasonable job of predicting the measured ice shapes. For any given experimental condition, one of the three codes predicted the general ice features (i.e., shape, impingement limits, mass of ice) somewhat better than did the other two. However, no single code consistently did better than the other two over the full range of conditions examined, which included rime, mixed, and glaze ice conditions. In several of the cases, DRA showed that the user's knowledge of icing can significantly improve the accuracy of the code prediction. Rime ice predictions were reasonably accurate and consistent among the codes, because droplets freeze on impact and the freezing model is simple. Glaze ice predictions were less accurate and less consistent among the codes, because the freezing model is more complex and is critically dependent...

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1430

Book Description


Advisory Circular

Advisory Circular PDF Author: United States. Federal Aviation Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32

Book Description


Ice Accretion and Icing Technology

Ice Accretion and Icing Technology PDF Author: Robert J Flemming
Publisher: SAE International
ISBN: 0768081203
Category : Technology & Engineering
Languages : en
Pages : 122

Book Description
The effects of inflight atmospheric icing can be devastating to aircraft. Universities and industry have been hard at work to respond to the challenge of maintaining flight safety in all weather conditions. Proposed changes in the regulations for operation in icing conditions are sure to keep this type of research and development at its highest level. This is especially true for the effects of ice crystals in the atmosphere, and for the threat associated with supercooled large drop (SLD) icing. This collection of ten SAE International technical papers brings together vital contributions to the subject. Icing on aircraft surfaces would not be a problem if a material were discovered that prevented the freezing and accretion of supercooled drops. Many options that appeared to have promising icephobic properties have had serious shortfalls in durability. This title addresses, among other topics, the measurement techniques and the drop physics that apply to icing, certification for flight through ice crystal clouds and in supercooled large drops, improvements in predictive techniques, scaling methods, test facilities and techniques, and rotorcraft icing.