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

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

2081. Stability. Langley full-scale tunnel investigation of factors affecting directional stability and trim characteristics of fighter-type airplane [with list of references]; by Harold H. Sweberg, Eugene R. Guryansky, and Roy H. Lange.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-109

2082. Stability. Notes on propeller and slipstream in relation to stability [with list of references]; by Herbert S. Ribner.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-25

2083. Stability. Stability and control characteristics of fighter airplane in inverted flight attitude as determined by model tests [with list of references]; by John W. Paulson and Charles V. Bennett.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 4.N 21/5:11/L-15

2084. Stability. Stability of body stabilized by fins and suspended from airplane [with list of references]; by W. H. Phillips.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-28

2085. Stability. Wind-tunnel procedure for determination of critical stability and control characteristics of airplanes [with list of references]; by Harry J. Goett, Roy P. Jackson, and Steven E. Belsley.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/W-5

2086. Static pressure. Effect of Mach number on position error as applied to pitotstatic tube located 0.55 chord ahead of airplane wing [with list of references]; by W. F. Lindsey.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-75

2087. Static pressure. Flight investigation at high Mach numbers of several methods of measuring static pressure on airplane wing [with one reference]; by John A. Zalovcikand Fred L Daum.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-90

2088. Stick-fixed neutral points. Effect of power on stick-fixed neutral points of several single-engine monoplanes as determined in flight; by Maurice D. White.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-24

2089. Stick-force characteristics. Use of variable-ratio geared tabs to improve stickforce characteristics in turning flight [with one reference]: by Harold F. Kleckner.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-85

2090. Stick-free neutral points. Some notes on determination of stick-free neutral point from wind-tunnel data [with list of references]; by Marvin Schuldenfrei.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-251

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