Towing Tests Of Models As An Aid In The Design Of Seaplanes
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Author | : P. Schröder |
Publisher | : |
Total Pages | : 664 |
Release | : 1932 |
Genre | : Marine towing |
ISBN | : |
This report concerns the making and evaluation of a towing test of a seaplane float system. Some of the topics considered are: 1) the influence of the wing cell and power plant on the take-off performance; 2) the determination of the resistance curve for the take-off free to trim; 3) the resistance curves with elevator control (at fixed trims); 4) take-off time and take-off run.
Author | : |
Publisher | : |
Total Pages | : 790 |
Release | : 1932 |
Genre | : Aeronautics |
ISBN | : |
Chiefly translations from foreign aeronautical journals.
Author | : Eastman Nixon Jacobs |
Publisher | : |
Total Pages | : 190 |
Release | : 1933 |
Genre | : Aerofoils |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 724 |
Release | : 1942 |
Genre | : Aeronautics |
ISBN | : |
Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 222 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 586 |
Release | : |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 616 |
Release | : 1949 |
Genre | : Aeronautics |
ISBN | : |
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 332 |
Release | : 1932 |
Genre | : Aeronautics |
ISBN | : |
Chiefly translations from foreign aeronautical journals.
Author | : H. Weinhart |
Publisher | : |
Total Pages | : 574 |
Release | : 1939 |
Genre | : Automobiles |
ISBN | : |
Engine knock is, as is known, preceded by normal burning of the first part of the charge, and only the part burned last (residual charge), knocks. The aim of the present measurements was, first, to reexamine the combustion form in this residual charge, because of the absence of uniform and frequently contradictory results in the very extensive literature on the subject. On top of that, an attempt was to be made to gain a deeper insight into the mechanism accompanying the combustion process, by means of the electrical test equipment perfected in recent years.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 312 |
Release | : 1936 |
Genre | : Aeronautics |
ISBN | : |