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Y 3.N 21/5:6/2770
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Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers / |
1 |
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Y 3.N 21/5:6/2771
|
Thermal buckling of plates / |
1 |
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Y 3.N 21/5:6/2772
|
Driving standing waves by heat addition / |
1 |
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Y 3.N 21/5:6/2773
|
An approximate method for determining the displacement effects and viscous drag of laminar boundary layers in two-dimensional hypersonic flow / |
1 |
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Y 3.N 21/5:6/2774
|
A method for finding a least-squares polynomial that passes through a specified point with specified derivatives / |
1 |
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Y 3.N 21/5:6/2775
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Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6 / |
1 |
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Y 3.N 21/5:6/2776
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The effect of a simulated propeller slipstream on the aerodynamic characteristics of an unswept wing panel with and without nacelles at Mach numbers from 0.30 and 0.86 / |
1 |
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Y 3.N 21/5:6/2777
|
Theoretical distribution of slip angles in an aggregate of face-centered cubic crystals / |
1 |
|
Y 3.N 21/5:6/2778
|
Stress and strain at onset of crazing of polymethyl methacrylate at various temperatures / |
1 |
|
Y 3.N 21/5:6/2779
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Effects of moderate biaxial stretch-forming on tensile and crazing properties of acrylate plastic crazing / |
1 |
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Y 3.N 21/5:6/2780
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Flight investigation of transient wing response on a four-engine bomber airplane in rough air with respect to center-of-gravity accelerations / |
1 |
|
Y 3.N 21/5:6/2781
|
The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives / |
1 |
|
Y 3.N 21/5:6/2782
|
Bending of thin plates with compound curvature / |
1 |
|
Y 3.N 21/5:6/2783
|
Use of a consolidated porous medium for measurement of flow rate and viscosity of gases at elevated pressures and temperatures / |
1 |
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Y 3.N 21/5:6/2784
|
Method for calculation of compressible laminar boundary-layer characteristics in axial pressure gradient with zero heat transfer / |
1 |
|
Y 3.N 21/5:6/2785
|
Introduction to electrical-circuit analogies for beam analysis / |
1 |
|
Y 3.N 21/5:6/2786
|
Equivalent plate theory for a straight multicell wing / |
1 |
|
Y 3.N 21/5:6/2787
|
Airfoil profiles for minimum pressure drag at supersonic velocities - application of shock-expansion theory, including consideration of hypersonic range / |
2 |
|
Y 3.N 21/5:6/2788
|
Effects of solvents in improving boundary lubrication of steel by silicones / |
1 |
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Y 3.N 21/5:6/2789
|
Some dynamic effects of fuel motion in simplified model tip tanks on suddenly excited bending oscillations / |
1 |
