Andrews, Sydney Thomas Giles, Benson, Sydney Frederick · New York, E.P. Dutton & Company · leaf 251
226 AEROPLANE DESIGN plasticine and the drag at zero yawing angle determined. The drag was found to be reduced from 0*016 Ib. to 0*0148 lb., a reduction of 7*5%. The general results indicate that model, Fig. 169, is slightly better than the B.E. 2, but not so good as the B.E. 3 body. The curves of… … Rg. 170 for displacements from the symmetrical position as regards yawing motion about the C.G. This is probably due to the two small fins just in front of the rudder itself, which were not removed in the test without the rudder. In Table XXXI II. the resistance in pounds of the four full- sized…
Airplanes -- Design and construction · Airplanes
Internet Archive · University of California Libraries · Public domain (published before 1931). Free to use for anything.
