The effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane /

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Bibliographic Details
Main Author: Wallace, Rudolf N. (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) ; 475.
Subjects:
Online Access:CONNECT

MARC

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245 1 4 |a The effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane /  |c by Rudolf N. Wallace. 
264 1 |a Washington, [D.C.] :  |b National Advisory Committee for Aeronautics,  |c 1933. 
300 |a 1 online resource (8 pages, 8 unnumbered pages) :  |b illustrations. 
336 |a text  |b txt  |2 rdacontent 
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490 1 |a Technical note / National Advisory Committee for Aeronautics ;  |v No. 475 
588 |a Description based on online resource, PDF version; title from title page (TRAIL, viewed January 28, 2021). 
500 |a "November, 1933." 
500 |a No Federal Depository Library Program (FDLP) item number. 
504 |a Includes bibliographical references (page 7). 
650 0 |a Airplanes  |x Wings. 
650 0 |a Split flaps (Airplanes) 
650 0 |a Wind tunnel testing. 
650 7 |a Airplanes  |x Wings.  |2 fast  |0 (OCoLC)fst00803545 
650 7 |a Split flaps (Airplanes)  |2 fast  |0 (OCoLC)fst01743451 
650 7 |a Wind tunnel testing.  |2 fast  |0 (OCoLC)fst01744047 
710 1 |a United States.  |b National Advisory Committee for Aeronautics,  |e issuing body. 
776 0 8 |i Print version:  |a Wallace, Rudolf N.  |t Effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane  |w (OCoLC)644259240 
830 0 |a Technical note (United States. National Advisory Committee for Aeronautics) ;  |v 475. 
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