Y 3.N 21/5:6/3277
|
Space heating rates for some premixed turbulent propane-air flames / |
1 |
Y 3.N 21/5:6/3278
|
Attenuation in a shock tube due to unsteady-boundary-layer action / |
1 |
Y 3.N 21/5:6/3279
|
Effect of phosphate coatings on temperature of metal parts exposed to flame environments / |
1 |
Y 3.N 21/5:6/3280
|
Electrical analogies for stiffened shells with flexible rings / |
1 |
Y 3.N 21/5:6/3281
|
Intergranular corrosion of high-purity aluminum in hydrochloric acid. |
1 |
Y 3.N 21/5:6/3282
|
Intergranular corrosion of high-purity aluminum in hydrochloric acid. : 2- Grain-boundary segregation of impurity atoms / |
1 |
Y 3.N 21/5:6/3283
|
Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section / |
2 |
Y 3.N 21/5:6/3284
|
Examination of the existing data on the heat transfer of turbulent boundary layers at supersonic speeds from the point of view of Reynolds analogy / |
1 |
Y 3.N 21/5:6/3285
|
Section characteristics of an NACA 0006 airfoil with area suction near the leading edge / |
1 |
Y 3.N 21/5:6/3286
|
Generalized indicial forces on deforming rectangular wings in supersonic flight / |
1 |
Y 3.N 21/5:6/3287
|
Heat transfer from a hemisphere-cylinder equipped with flow-separation spikes / |
1 |
Y 3.N 21/5:6/3288
|
On the analysis of linear and nonlinear dynamical systems from transient-response data / |
1 |
Y 3.N 21/5:6/3289
|
The minimization of wave drag for wings and bodies with a given base area or volume / |
1 |
Y 3.N 21/5:6/3290
|
On the minimization of airplane responses to random gusts / |
1 |
Y 3.N 21/5:6/3291
|
Experimental investigation of notch-size effects on rotating-beam fatigue behavior of 75S-T6 aluminum alloy / |
1 |
Y 3.N 21/5:6/3292
|
Influence of exposed area on stress-corrosion cracking of 24S aluminum alloy / |
1 |
Y 3.N 21/5:6/3293
|
Cumulative fatigue damage of axially loaded Alclad 75S-T6 and Alclad 24S-T3 aluminum-alloy sheet / |
1 |
Y 3.N 21/5:6/3294
|
Friction study of aircraft tire material on concrete / |
1 |
Y 3.N 21/5:6/3295
|
Effect of pressure on thermal conductance of contact joints / |
1 |
Y 3.N 21/5:6/3296
|
Separation, stability, and other properties of compressible boundary layer with pressure gradient and heat transfer / |
1 |