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Y 3.N 21/5:6/1734
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Investigation of the variation of maximum lift for a pitching airplane model and comparison with flight results / |
1 |
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Y 3.N 21/5:6/1735
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Performance of exhaust-gas blowdown turbine and various engine systems using a 12-cylinder liquid-cooled engine / |
1 |
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Y 3.N 21/5:6/1736
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Theoretical method for solution of aerodynamic forces on thin wings in nonuniform supersonic stream with an application to tail surfaces / |
1 |
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Y 3.N 21/5:6/1737
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Effect of variation in diameter and pitch of rivets on compression strength of panels with Z-section stiffeners. : Panels that fail by local buckling and have various values of width-to-thickness ratio for the webs of the stiffeners / |
1 |
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Y 3.N 21/5:6/1738
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Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model / |
1 |
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Y 3.N 21/5:6/1739
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Comparison with experiment of several methods of predicting the lift of wings in subsonic compressible flow / |
1 |
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Y 3.N 21/5:6/1740
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An Approximate determination of the lift of slender cylindrical bodies and wing-body combinations at very high supersonic speeds / |
1 |
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Y 3.N 21/5:6/1741
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Exploratory wind-tunnel investigation of the effectiveness of area suction in eliminating leading-edge separatioin over an NACA 64₁A212 airfoil / |
1 |
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Y 3.N 21/5:6/1742
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Stability and control characteristics at low speed of an airplane model having a 38.7 degree sweptback wing with aspect ratio 4.51, taper ratio 0.54, and conventional tail surfaces / |
1 |
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Y 3.N 21/5:6/1743
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Flight measurements of the stability, control, and stalling characteristics of an airplane having a 35 degree sweptback wing without slots and with 80-percent-span slots and a comparison with wind-tunnel data / |
1 |
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Y 3.N 21/5:6/1744
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Two-dimensional compressible flow in conical mixed-flow compressors / |
1 |
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Y 3.N 21/5:6/1745
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Theoretical evaluation of the ducted-fan turbojet engine / |
1 |
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Y 3.N 21/5:6/1746
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Flow of a compressible fluid past a symmetrical airfoil in a wind tunnel and in free air / |
1 |
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Y 3.N 21/5:6/1747
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Determination of coupled and uncoupled modes and frequencies of natural vibration of swept and unswept wings from uniform cantilever modes / |
1 |
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Y 3.N 21/5:6/1748
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Calculation of tunnel-induced upwash velocities for swept and yawed wings / |
1 |
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Y 3.N 21/5:6/1749
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Shear flows in multicell sandwich sections / |
1 |
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Y 3.N 21/5:6/1750
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Buckling tests of flat rectangular plates under combined shear and longitudinal compression / |
1 |
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Y 3.N 21/5:6/1751
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Buckling of a long square tube in torsion and compression / |
1 |
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Y 3.N 21/5:6/1752
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Jet-boundary-induced-upwash velocities for swept reflection-plane models mounted vertically in 7- by 10-foot, closed, rectangular wind tunnels / |
1 |
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Y 3.N 21/5:6/1753
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Evaluation of a fixed spoiler as a gust alleviator / |
1 |
