|
Y 3.N 21/5:6/4376
|
Analytical and experimental investigation of temperature recovery factors for fully developed flow of air in a tube / |
1 |
|
Y 3.N 21/5:6/4377
|
Use of the Coanda Effect for jet deflection and vertical lift with multiple-flat-plate and curved-plate deflection surfaces / |
1 |
|
Y 3.N 21/5:6/4378
|
Preliminary heat-transfer studies on two bodies of revolution at angle of attack at a Mach number of 3.12 / |
1 |
|
Y 3.N 21/5:6/4379
|
Torque-speed characteristics for high-specific-work turbines / |
1 |
|
Y 3.N 21/5:6/4380
|
Approximate method for calculation of laminar boundary layer with heat transfer on a cone at large angle of attack in supersonic flow / |
1 |
|
Y 3.N 21/5:6/4381
|
Effect of pressure and duct geometry on bluff-body flame stabilization / |
1 |
|
Y 3.N 21/5:6/4382
|
Investigation of boiling burnout and flow stability for water flowing in tubes / |
1 |
|
Y 3.N 21/5:6/4383
|
A cooled-gas pyrometer for use in high-temperature gas streams / |
1 |
|
Y 3.N 21/5:6/4384
|
Analysis of turbulent flow and heat transfer in noncircular passages / |
1 |
|
Y 3.N 21/5:6/4385
|
Comparison of shock-expansion theory with experiment for the lift, drag, and pitching-moment characteristics of two wing-body combinations at M = 5.0 / |
1 |
|
Y 3.N 21/5:6/4386
|
An analysis of ramjet engines using supersonic combustion / |
1 |
|
Y 3.N 21/5:6/4387
|
Experimental evaluation of low-band-pass landing-gear shock absorber for pulse loadings / |
1 |
|
Y 3.N 21/5:6/4388
|
Effects of nose angle and Mach number on transition on cones at supersonic speeds / |
1 |
|
Y 3.N 21/5:6/4389
|
Effect of advance ratio on flight performance of a modified supersonic propeller / |
1 |
|
Y 3.N 21/5:6/4390
|
Effects of frequency and amplitude on the yawing derivatives of triangular, swept, and unswept wings and of a triangular-wing-fuselage combination with and without a triangular tail performing sinusoidal yawing oscillations / |
1 |
|
Y 3.N 21/5:6/4391
|
Mass transfer cooling near the stagnation point / |
1 |
|
Y 3.N 21/5:6/4392
|
A theoretical study of stagnation-point ablation / |
1 |
|
Y 3.N 21/5:6/4393
|
Some static longitudinal stability characteristics of an overlapped-type tandem-rotor helicopter at low airspeeds / |
1 |
|
Y 3.N 21/5:6/4394
|
The rate of fatigue-crack propagation in two aluminum alloys / |
1 |
|
Y 3.N 21/5:6/4395
|
Use of the kernel function in a three-dimensional flutter analysis with application to a flutter-tested delta-wing model / |
1 |
