Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /

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Bibliographic Details
Main Author: Heald, R. H. (Author)
Format: Government Document Electronic eBook
Language:English
Published: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1933.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 441.
Subjects:
Online Access:CONNECT

MARC

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245 1 0 |a Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /  |c by R.H. Heald. 
264 1 |a Washington, [D.C.] :  |b National Advisory Committee for Aeronautics,  |c 1933. 
300 |a 1 online resource (12 pages, 3 unnumbered pages) :  |b illustrations. 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a Technical note / National Advisory Committee for Aeronautics ;  |v No. 441 
588 |a Description based on online resource, PDF version; title from title page (TRAIL, viewed January 8, 2021). 
500 |a "January, 1933." 
500 |a No Federal Depository Library Program (FDLP) item number. 
504 |a Includes bibliographical references (page 12). 
650 0 |a Ailerons. 
650 0 |a Flaps (Airplanes) 
650 0 |a Rolling (Aerodynamics) 
650 0 |a Yawing (Aerodynamics) 
650 0 |a Hinge moments (Aerodynamics) 
650 0 |a Wind tunnel testing. 
650 7 |a Hinge moments (Aerodynamics)  |2 fast  |0 (OCoLC)fst00957213 
650 7 |a Rolling (Aerodynamics)  |2 fast  |0 (OCoLC)fst01099689 
650 7 |a Wind tunnel testing.  |2 fast  |0 (OCoLC)fst01744047 
650 7 |a Yawing (Aerodynamics)  |2 fast  |0 (OCoLC)fst01182552 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
776 0 8 |i Print version:  |a Heald, R. H.  |t Rolling, yawing, and hinge moments produced by rectangular ailerons  |w (OCoLC)643562889 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v 441. 
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