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

2091. Spin (aircraft). Mass-distribution criterion for predicting effect of control manipulation on recovery from spin [with one reference]; by A. I. Neihouse.

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-168

2092. Spin (aircraft). Spin-tunnel tests of airplane models with extreme variations in mass distribution along three body axes [with list of references]; by Robert W. Kamm.

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-22

2093. Spoilers. Wind-tunnel tests of spoilers on tail surfaces [with list of references]; by Robert B. Liddell.

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-260

2094. Stability. Analytical investigation of effects of elevator-fabric distortion on longitudinal stability and control of airplane [with list of references]; by Charles W. Mathews.

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-142

2095. Stability. Comparison of wind-tunnel and flight measurements of stability and control characteristics of Douglas A-26 airplane [with list of references]; by Gerald G. Kayten and William Koven.

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-99

2096. Stability. Determination of stability and control characteristics of straight-wing, tailless fighter-airplane model in Langley free-flight tunnel [with list of references]; by Charles L. Seacord, jr., and Herman O. Ankenbruck.

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-199

2097. Stability. Determination of stability and control characteristics of tailless all-wing airplane model with sweepback in Langley 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:: [1946.]
SuDoc number:: Y 3.N 21/5:11/L-50

2098. Stability. Effect of lateral area on lateral stability and control characteristics of airplane as determined by tests of model in Langley free-flight tunnel [with list of references]; by Hubert M. Drake.

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-103

2099. Stability. Effect of powered propellers on aerodynamic characteristics and porpoising stability of dynamic model of long-range flying boat [with one reference]; by Norman S. Land.

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-235

2100. Stability. Effect of spring and gravity moments in control system on longitudinal stability of Brewster XSBA-1 airplane [with one reference]; by William 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-263

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