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Full scale determination of the lift and drag of a seaplane

Author
Munk, Max M
Physical Description
1 electronic document
Online Version

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Summary
The speed, barometric pressure, and number of revolutions of the engine of a seaplane were measured, including tests with stopped engine. The mean data obtained are given in the following note; the results of the gliding tests are used for the computation of the lift and drag coefficients, and by making use of them the results of the engine flights are used for the computation of the propeller efficiency.
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 19930080873.
Accession ID: 93R10163.
NACA-TN-92.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15666802