Author : C. S. Draper
Publisher :
Page : 76 pages
File Size : 13,49 MB
Release : 1934
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 670 pages
File Size : 41,93 MB
Release : 1934
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : pages
File Size : 48,49 MB
Release : 1937
Category : Aeronautics
ISBN :
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author : James M. Shoemaker
Publisher :
Page : 530 pages
File Size : 35,84 MB
Release : 1934
Category : Planing hulls
ISBN :
This report presents towing tests made in the N.A.C.A. tank of a parent form and five variations of a flying-boat hull. The beams of two of the dervied forms were made the same as that of the parent and the lengths changed by increasing and decreasing the spacing of stations. The lengths of two other of the derived forms were made the same as that of the parent while the beams were changed by increasing and decreasing the spacing of buttocks, all other widths being changed in proportion. The remaining derived form has the same length and beam as the parent, but the lines of the forebody were altered to give a planing bottom with no longitudinal curvature forward of the step.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 40 pages
File Size : 27,88 MB
Release : 1941
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 780 pages
File Size : 30,10 MB
Release :
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 590 pages
File Size : 28,38 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 80 pages
File Size : 43,98 MB
Release : 1945
Category : Aeronautics
ISBN :
Author : M. Kramer
Publisher :
Page : 754 pages
File Size : 19,71 MB
Release : 1951
Category : Ailerons
ISBN :
The present report describes the development of spoiler control at the DVL from the end of 1936 until the beginning of 1939. The authors are fully aware that the present report also forms only a contribution to the problem of spoiler control and offers at best a possibility of extrapolation regarding the behavior of the control in modern airplanes. A modern airplane (ME 109) is being reconstructed for conversion to spoiler control. Experience has shown, however, that the construction and testing of such a model requires at least a year. Thus it seems appropriate to report summarily now in order to keep the understanding and cooperation of the interested departments aroused. The following reports are only a section of a long development partly evolved abroad.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 120 pages
File Size : 48,63 MB
Release : 1945
Category : Aeronautics
ISBN :
