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Airfoil Sections for Flying Models/ Profili Alari per Modelli Volanti
RCL#2117

Airfoil Sections for Flying Models/ Profili Alari per Modelli Volanti - cover thumbnail  

"In comparing the results shown in this report with those obtained in other wind tunnels, one must consider the different surface roughness, the size tolerances of the sections, and the overall measurements accuracy of the MEG low speed wind tunnel."

Airfoil Sections for Flying Models/ Profili Alari per Modelli Volanti
ASA Test Report
Enrico Gallazzi
Associazione Sportiva Aeromodellistica, Milano, Italy
1972
Book, 23 pages

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About this title

"ASA Test Report 03-72"

Bi-lingual (Italian & English ) report from the Italian Associazione Sportiva Aeromodellistica.

Complementary to the "APPUNTI SUL PROGETTO AERODINAMICO DI MODELLI VOLANTI" (Notes on Aerodynamic Design of Flying Models). It presents real data curves of 16 airfoils, obtained in an experimental wind tunnel at Reynolds nr. as low as 57.000-60.000 and at attack angles between -2 ° and +8 º

More information about the author, Enrico Gallazzi: whttp://www.girellafly.net/gallazzi14/enrico.php


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Airfoil Sections for Flying Models/ Profili Alari per Modelli Volanti
Submission date: 16/03/2018
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TitleID: 2117 | Filesize: 6171KB
Credit*: JoanBrunet
Format: PDF
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