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An approximate spin design criterion for monoplanes, 1 May 1939

By Seidman, O.

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Book Id: WPLBN0002204667
Format Type: PDF eBook :
File Size: 0.8 MB
Reproduction Date: 2012

Title: An approximate spin design criterion for monoplanes, 1 May 1939  
Author: Seidman, O.
Volume:
Language: English
Subject: LIGHT AIRCRAFT, PROPULSIVE EFFICIENCY, THRUST
Collections: NASA Publication Collection
Historic
Publication Date:
1975
Publisher:

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O, S., & J, D. C. (1975). An approximate spin design criterion for monoplanes, 1 May 1939. Retrieved from http://www.ebooklibrary.org/


Description
Supplemental catalog subcollection information: NASA Publication Collection; Astrophysics and Technical Documents; An approximate empirical criterion, based on the projected side area and the mass distribution of the airplane, was formulated. The British

Summary
Contributor: National Aeronautics and Space Administration (NASA). The digitalization of this book was sponsored by National Aeronautics and Space Administration (NASA); Additional Subject Descriptions: LIGHT AIRCRAFT; PROPULSIVE EFFICIENCY; THRUST; PROPELLER EFFICIENCY; SPIN DYNAMICS; SPIN TESTS; TORQUE; WIND TUNNEL TESTS

 

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