Experimental investigation at low speed of the effects of wing position on the static stability of models having fuselages of various cross section and unswept and 45 degree sweptback surfaces / William Letko.

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Bibliographic Details
Main Author: Letko, William
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1956.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3857.
Subjects:

MARC

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100 1 |a Letko, William. 
245 1 0 |a Experimental investigation at low speed of the effects of wing position on the static stability of models having fuselages of various cross section and unswept and 45 degree sweptback surfaces /  |c William Letko. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1956. 
300 |a 77 pages :  |b illustrations ;  |c 27 cm. 
336 |a text  |b txt  |2 rdacontent. 
337 |a unmediated  |b n  |2 rdamedia. 
338 |a volume  |b nc  |2 rdacarrier. 
490 1 |a National Advisory Committee for Aeronautics ;  |v 3857. 
500 |a "November 1956." 
500 |a NACA TN Number 3857. 
504 |a Includes bibliographical references. 
520 3 |a An experimental investigation was made to determine the effects of wing position on the low-speed static longitudinal and static lateral stability derivatives of airplane models having fuselages of square and rectangular cross sections and unswept and 45 degree sweptback surfaces. The horizontal tail of each model was located on the fuselage center line. 
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650 0 |a Airplanes  |x Models  |x Testing. 
650 0 |a Stability of airplanes, Lateral.  |0 http://id.loc.gov/authorities/subjects/sh85127187. 
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650 7 |a Stability of airplanes, Lateral.  |2 fast  |0 (OCoLC)fst01131215. 
650 7 |a Stability of airplanes, Longitudinal.  |2 fast  |0 (OCoLC)fst01131217. 
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