Elevator stick forces in spins as computed from wind-tunnel measurements / by Oscar Seidman and J.W. Klinar.

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Bibliographic Details
Main Author: Seidman, Oscar
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Klinar, J. W.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L422.
Subjects:

MARC

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100 1 |a Seidman, Oscar.  |0 http://id.loc.gov/authorities/names/no2006103703  |1 http://isni.org/isni/0000000048850240. 
245 1 0 |a Elevator stick forces in spins as computed from wind-tunnel measurements /  |c by Oscar Seidman and J.W. Klinar. 
246 3 |a NACA Wartime Reports. Series L. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c [1942] 
300 |a 9 pages, 14 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 Wartime Report / National Advisory Committee for Aeronautics ;  |v no. L422. 
500 |a NACA Wartime Report L-422. 
500 |a Originally issued as NACA as an Advance Restricted Report (October 1942) 
500 |a Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia. 
504 |a Includes bibliographical references. 
520 3 |a Data from wind-tunnel measurements of elevator hinge-moment coefficients at high angle of attack are utilized in estimating elevator stick forces in spins. 
520 3 |a The analysis indicates that elevator forces on several current airplanes will be so high that the pilot will be unable to push the stick to the neutral position. Large nose balances involve danger of the elevator locking in the full-up position. Trimming tabs can be used to reduce the elevator stick force. Stick forces will be greater in steep spins than in flat spins. 
650 0 |a Airplanes  |x Control. 
650 0 |a Elevators (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh85042561. 
650 0 |a Spin (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85126648. 
650 0 |a Wind tunnel testing.  |0 http://id.loc.gov/authorities/subjects/sh2007008292. 
650 0 |a Charts, diagrams, etc.  |0 http://id.loc.gov/authorities/subjects/sh87002373. 
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650 7 |a Charts, diagrams, etc.  |2 fast  |0 (OCoLC)fst00852545. 
650 7 |a Elevators (Airplanes)  |2 fast  |0 (OCoLC)fst00908089. 
650 7 |a Spin (Aerodynamics)  |2 fast  |0 (OCoLC)fst01129803. 
650 7 |a Wind tunnel testing.  |2 fast  |0 (OCoLC)fst01744047. 
700 1 |a Klinar, J. W. 
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. 
710 2 |a Langley Aeronautical Laboratory.  |0 http://id.loc.gov/authorities/names/n81018841. 
830 0 |a Wartime Reports (United States. National Advisory Committee for Aeronautics) ;  |v no. L422. 
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