A simple method for increasing the lift of airplane wings by means of flaps / by Eugen Gruschwitz and Oskar Schrenk.

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Bibliographic Details
Main Author: Gruschwitz, E. (Eugen)
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Schrenk, Oskar
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Commitee for Aeronautics, 1933.
Series:Technical memorandum (United States. National Advisory Committee for Aeronautics) ; no. 714.
Subjects:

MARC

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245 1 2 |a A simple method for increasing the lift of airplane wings by means of flaps /  |c by Eugen Gruschwitz and Oskar Schrenk. 
260 |a Washington, D.C. :  |b National Advisory Commitee for Aeronautics,  |c 1933. 
300 |a 5 pages, 5 unnumbered 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 Technical memorandums ;  |v no. 714. 
500 |a "June 1933." 
500 |a NACA TM Number 714. 
500 |a Translated from Zeitschrift fur Flugtechnik und Motorluftschiffahrt. Volume 23, Number 20, pp. 597-601, October 28, 1932, by the National Advisory Commitee for Aeronautics. 
500 |a Abstract of a lecture by Oskar Schrenk at the twenty-first annual meeting of the W.G.L. (Wissenschaftliche Gesellschaft fur Luftfahrt), 1932. 
504 |a Includes bibliographical references. 
520 3 |a Aerodynamic considerations led us, not long ago, to investigate a device which seemed to promise a contribution to the problem of reducing the landing speed of an airplane. We have subsequently learned that similar devices had already been proposed and investigated by others, but it seems advisable, nevertheless, to report our results. The problem is to create, in landing, a region of turbulence on the lower side of the wing near the trailing edge by some obstacle to the air flow. The devices tested by us consisted of flaps of varying chord and position, the chord s being equal to the distance of the pivot from the trailing edge. 
650 0 |a Airplanes  |x Wings.  |0 http://id.loc.gov/authorities/subjects/sh85002923. 
650 0 |a Lift (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85076855. 
650 0 |a Flaps (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh85049001. 
650 7 |a Airplanes  |x Wings.  |2 fast  |0 (OCoLC)fst00803545. 
650 7 |a Flaps (Airplanes)  |2 fast  |0 (OCoLC)fst00927038. 
650 7 |a Lift (Aerodynamics)  |2 fast  |0 (OCoLC)fst00998431. 
700 1 |a Schrenk, Oskar. 
710 1 |a United States.  |b National Advisory Committee for Aeronautics.  |0 http://id.loc.gov/authorities/names/n79060141  |1 http://isni.org/isni/0000000106642010. 
830 0 |a Technical memorandum (United States. National Advisory Committee for Aeronautics) ;  |v no. 714.  |0 http://id.loc.gov/authorities/names/no2009014150. 
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