Y3.N21_5..5_771
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Review of flight tests of NACA C and D cowlings on the XP-42 airplane. |
1 |
Y3.N21_5..5_772
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Determination of general relations for the behavior of turbulent boundary layers. |
1 |
Y3.N21_5..5_773
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Analysis of heat and compressibility effects in internal flow systems and high-speed tests of a ram-jet system. |
1 |
Y3.N21_5..5_774
|
Effect of tilt of the propeller axis on the longitudinal-stability characteristics of single-engine airplanes. |
1 |
Y3.N21_5..5_776
|
The theory of propellers, II method for calculating the axial interference velocity. |
1 |
Y3.N21_5..5_777
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The theory of propellers, III-the slipstream contraction with numerical values for two-blade and four-blade propellers. |
1 |
Y3.N21_5..5_778
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The theory of propellers, IV-thrust, energy, and efficiency formulas for single- and dual-rotating propellers with ideal circulation distribution. |
1 |
Y3.N21_5..5_779
|
The effect of increased cooling surface on performance of aircraft-engine cylinders as shown by tests of the NACA cylinder. |
1 |
Y3.N21_5..5_780
|
Compressible potential flow with circulation about a circular cylinder. |
1 |
Y3.N21_5..5_781
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Wind-tunnel procedure for determination of critical stability and control characteristics of airplanes. |
1 |
Y3.N21_5..5_782
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Wall interference in a two-dimensional-flow wind tunnel, with consideration of the effect of compressibility. |
1 |
Y3.N21_5..5_783
|
Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel. |
1 |
Y3.N21_5..5_784
|
Intercooler cooling-air weight flow and pressure drop for minimum drag loss. |
1 |
Y3.N21_5..5_785
|
Preknock vibrations in a spark-ignition engine cylinder as revealed by high-speed photography. |
1 |
Y3.N21_5..5_787
|
A theoretical investigation of the rolling oscillations of an airplane with ailerons free. |
1 |
Y3.N21_5..5_791
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A theoretical investigation of longitudinal stability of airplanes with free controls including effect of friction in control system. |
1 |
Y3.N21_5..5_792
|
Flight studies of the horizontal-tail loads experienced by a fighter airplane in abrupt maneuvers. |
1 |
Y3.N21_5..5_793
|
Experiments on drag of revolving disks, cylinders, and streamline rods at high speeds. |
1 |
Y3.N21_5..5_794
|
The flow of a compressible fluid past a circular arc profile. |
1 |
Y3.N21_5..5_795
|
The NACA impact basin and water landing tests of a float model at various velocities and weights. |
1 |