Publish Year Decade: 1940 - 1949 / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Publish Year Decade 1940 - 1949 Sudoc Stem Y 3.N 21/5

2011. Load (mechanics). Effect of high wing loading on landing technique and distance, with experimental data for B-26 airplane [with list of references]; by F. B. Gustafson and William J. O'Sullivan, jr.

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-160

2012. Load (mechanics). Extended tables of stiffness and carry-over factor for structural members under axial load [with list of references]; by Eugene E. Lundquist and W. D. Kroll.

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-255

2013. Load (mechanics). Flight studies of horizontal-tail loads experienced by modern pursuit airplane in abrupt maneuvers; by Flight Research Maneuvers Section.

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-93

2014. Load (mechanics). In-line aircraft-engine bearing loads: 2, Blade-bearing loads [with list of references]; by Milton C. Shaw and E. Fred Macks.

Corporate/Agency Authors:: National Advisory Committee for Aeronautics
Publisher:: National Advisory Committee for Aeronautics
Date:: [1946.]
SuDoc number:: Y 3.N 21/5:11/E-46

2015. Load (mechanics). Relation between spanwise variations in critical Mach number and spanwise load distributions [with list of references]; by Richard T. Whitcomb.

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-182

2016. Load (mechanics). Theoretical and experimental dynamic loads for prismatic float having angle of dead rise of 22½° [with list of references]; by Wilbur L. Mayo.

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-70

2017. Load (mechanics). Theoretical distribution of load over swept-back wing [with list of references]; by Doris Cohen.

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-221

2018. Load (mechanics). Variation of hydrodynamic impact loads with flight-path angle for prismatic float at 3° trim and with 22½° angle of dead rise [with one reference]; by Sidney A. Batterson.

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-211

2019. Load (mechanics). Variation of hydrodynamic impact loads with flight-path angle for prismatic float at 6° and 9° trim and 22½° angle of dead rise [with list of references]; by Sidney A. Batterson and Thelma Stewart.

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-69

2020. Load (mechanics). Variation ol hydrodynamic impact loads with flight-path angle for prismatic float at 12° trim and with 22V2° angle of dead rise [with list of references]; by Sidney A. Batterson.

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-68

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