This report presents the attempt to develop a law which will permit the use of results obtained on small models in a tunnel for the calculation of full-sized airplanes, or if it exists, a law of similitude relating air forces on a full-sized plane to those on a reduced scale model.
Applying the results of experiments on small models in the wind tunnel to the calculation of full-sized aircraft
Congres International de la Navigation Aerienne (1st : 1921 : Paris, France)
1922-04-01
Sonstige
Keine Angabe
Englisch
Aircraft Wind Tunnel Characterization using Modern Design of Experiments
British Library Conference Proceedings | 2013
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