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Graphic method for calculating the speed and climbing ability of airplanes / by Adolf Rohrbach and Edwin Lupberger.

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Format:
Book
Government document
Author/Creator:
Rohrbach, Adolf, author.
Lupberger, Edwin, author.
Contributor:
United States. National Advisory Committee for Aeronautics, issuing body.
Series:
Technical note (United States. National Advisory Committee for Aeronautics) ; 163.
Technical notes / National Advisory Committee for Aeronautics ; No. 163
Language:
English
Subjects (All):
Airplanes--Handling characteristics.
Airplanes.
Graphic methods.
graphs.
Physical Description:
1 online resource (9 pages, 1 unnumbered page) : illustrations
Place of Publication:
[Washington, D.C.] : National Advisory Committee for Aeronautics, 1923.
Summary:
The simplest known methods for calculating airplane performances are those of Everling (Zeitschrift fur Flugtechnik und Motorluftschiffahrt, 1916, pages 125), and Kann (Technische Berichte, Vol. 1, No. 6, pp. 231). Both methods have this feature in common, that they express the particular quantity which is to be determined (time of climb, speed, et cetera) by a single formula. Thus, by using Everling's airplane calculation tables, we are able to find related values (e.g. gliding coefficient, ceiling, and total weight per horsepower), by a very simple graphical methods.
Notes:
Title from title screen (viewed August 9, 2019).
"October 1923."
"From Technische Berichte, Vol. III, No. 6."
"Translated by National Advisory Committee for Aeronautics"--Page 9
No Federal Depository Library Program (FDLP) item number.
Includes bibliographical reference (page 1).
Print version record.
Other Format:
Print version: Rohrbach, Adolf. Graphic method for calculating the speed and climbing ability of airplanes
OCLC:
1117765714

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