Author: National Advisory Committee for Aeronautics / Catalog Issue Year Decade: 1940 - 1949 - Blacklight Search Results

Start Over Author National Advisory Committee for Aeronautics Catalog Issue Year Decade 1940 - 1949

1211. Stability. Calculated effects of full-span slotted and Fowler flaps on longitudinal stability and control characteristics for typical fighter-type airplane with various tail modifications [with list of references]; by R. Fabian Goransou.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-392

1212. Stability. Comparison of predicted and actual control-fixed stability and control characteristics of Douglas A-26B airplane [with list of references]; by Harold L. Crane and Sigurd A. Sjoberg.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-608

1213. Stability. Compressibility effects on longitudinal stability and control of pursuit-type airplane as measured in flight [with list of references]; by William N. Turner, Paul J. Stelffen. and Lawrence A. Clousing.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/A-60

1214. Stability. Effect of angle of bend between plate elements on local instability of formed Z-sections [with list of references]; by J. Albert Roy and Evan H. Schuette.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-268

1215. Stability. Effect of changes in aspect radio, side area, flight-path angle, and normal acceleration on lateral stability [with list of references]; by M. J. Bamber.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-403

1216. Stability. Effect of mass distribution on lateral stability and control characteristics of airplane as determined by tests of model in free-flight tunnel [with list of references]; by John P. Campbell and Charles L. Seacord, jr.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-388

1217. Stability. Effect of wing loading and altitude on lateral stability and control characteristics of airplane as determined by tests of model in free-flight tunnel [with list of references]; by John P. Campbell and Charles L. Seacord, jr.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-522

1218. Stability. Free-flight-tunnel Investigation of effect of mode of propeller rotation upon lateral-stability characteristics of twin-engine airplane model with single vertical tails of different size [with list of references]; by Marvin Pitkin.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-354

1219. Stability. Full-scale tunnel investigation of control and stability of twin-engine monoplane with propellers operating [with list of references]; by Harold H. Sweberg.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-425

1220. Stability. Hydrodynamic-stability tests of model of flying boat and of planing surface having small downward projection (hook) on planing bottom near step [with list of references]; by James M. Benson.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1947.]
SuDoc number:: Y 3.N 21/5:11/L-518

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