ASME Transactions, 81. sējums,3. izdevumsAmerican Society of Mechanical Engineers., 1960 Vols. 2, 4-11, 62-68 include the Society's Membership list; v. 55-80 include the Journal of applied mechanics (also issued separately) as contributions from the Society's Applied Mechanics Division. |
No grāmatas satura
1.–3. rezultāts no 47.
309. lappuse
... least period T1 ; f ( y ) of least period To T1 . Select for h ( y ) a form which reduces the integrand in Equation ( 4 ) to a quartic in y so that the properties of elliptic functions could be used to fix a real period T1 . Frankly the ...
... least period T1 ; f ( y ) of least period To T1 . Select for h ( y ) a form which reduces the integrand in Equation ( 4 ) to a quartic in y so that the properties of elliptic functions could be used to fix a real period T1 . Frankly the ...
334. lappuse
... least when the ther- mal layer is fully developed , but it is possible that the absence of term corresponding to the pressure - velocity correlation is an in- dication of a fundamental difference in the two fluctuation fields . Corrsin ...
... least when the ther- mal layer is fully developed , but it is possible that the absence of term corresponding to the pressure - velocity correlation is an in- dication of a fundamental difference in the two fluctuation fields . Corrsin ...
665. lappuse
... least value at some values of a / d . It is known from the figure that the corresponding values of a / d becomes smaller when b / d is large and v small . If the maxi- = mum moment has its least value at a / d = 0 , and it increases ...
... least value at some values of a / d . It is known from the figure that the corresponding values of a / d becomes smaller when b / d is large and v small . If the maxi- = mum moment has its least value at a / d = 0 , and it increases ...
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advanced in papers amplitude analysis Applied Mechanics Division approximate ASME Applied Mechanics assumed axial axis beam bending bending moment boundary conditions boundary layer C₁ circular co-ordinates coefficients components computed constant corresponding cosh cross section curvature curve cylinder deflection deformation determined differential equations dimensionless Discussion displacement edge elastic equa equilibrium experimental expressions flow force frequency function gimbal given incremental initial integral isotropic JOURNAL OF APPLIED linear load Manuscript received material MECHANICAL ENGINEERS method mode motion nondimensional nonlinear normal obtained parameter photoelastic plane plastic plate Poisson's ratio pressure problem radial radius ratio received by ASME relations rotation shear shear stress shell shown in Fig sinh solution strain stress-strain T₁ temperature tension theory thickness tion torsion TRANS transverse turbulent understood as individual values vector velocity vibration wave yield surface zero дх