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31 The measurement technique of constant temperature anemometry was used to study experimentally the mechanism of drag reduction in turbulent boundary layer with riblet surface.

32 A method is proposed to calculated the incompressible three-dimensional turbulent boundary layer on both wall surfaces of vaneless diffusers.

33 The energy boundary layer integral method is applied to the thermal developing region of laminar falling liquid film over a vertical plate of constant heat flux.

34 A 3D integral boundary layer approach is used and coupled with streamline method for determining vortex-layer-type flow separation.

35 The bell reducer provides the cyclone action and the boundary layer control.

36 In the second part, we study the existence of boundary layer solutions to the Boltzmann equation with specular reflection and reverse reflection boundary conditions respectively.

37 The dispersion of chemically reactive species in the atmospheric boundary layer.

38 The results indicate that separation and reattachment occur on the boundary layer of the rocket because of the shock impinging with sharp changes in static pressure and temperature.

39 Besides, auto - ignition occurs in the boundary layer at the lower wall in many cases.

40 The bottom boundary layer under cnoidal waves was studied by using Acoustic Doppler Velocimeter(ADV) technique in a laboratory flume.

41 Ground effect has the very tremendous influence on boundary layer thickness, and air drag with underhood enhances 12%.

42 The result shows that the new model can simulate the turbulent structure and the cloud microphysical processes of the marine stratocumulus-topped planetary boundary layer.

43 Aerosol measurements in slant range in atmospheric boundary layer are performed by using a mobile pollution detecting lidar system (AML-1). The corresponding data processing method is introduced.

44 A careful chaotic dynamic analysis on a transitional boundary layer shows the existence of the strange attractor in the total transitional processes.

45 The - micron particle deposition is due to the thermophoretic force in boundary layer under high flow temperature.

46 The separating flow in a turbulent boundary layer was surveyed in a 2-D curved-wall diffuser by employing 2-D laser Doppler velometer.

47 An aeroelastic model for a UHV power transmission tower and its conductors was designed according to the law of similarity and tested in an atmospheric boundary layer wind tunnel.

48 Boundary layer phenomena of third - order nonlinear equation is studied in this paper.

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49 It is shown that an oncoming gravity wave interacts with localized mountain lee waves induced by topography to generate a viscous instability wave within the boundary layer.

50 The weak nonlinear instability of a nonparallel boundary layer is studied by nonlinear parabolized stability equations(PSE).

51 In order to minimize the boundary layer effects, the nozzles were made as short as possible.

52 This demonstrates that for propulsion-airframe integration, this genus of inlet would be advantageous in keeping the stability of boundary layer coming from the forebody .

53 The parabolized stability equations (PSEs) for high speed flows, especially supersonic and hypersonic flows, are derived and used to analyze the nonparallel boundary layer stability.

54 An error matching principle, which is base on the error analysis of the computations with high-aspect-ratio grids, is derived for the finite difference simulation of the viscous boundary layer flows.

55 A large frame schlieren image technique is presented in the paper. The technique has been applied to visualization of the boundary layer transition on the surface of the cone in the hypersonic flow.

56 The examples presented clearly show the effect of nonparallel flow on boundary layer stability.

57 In super critical Reynolds number range, flow asymmetry is induced by both the asymmetric vortices and asymmetric boundary layer state.

58 The turbulent characteristics in convective boundary layer topped temperature inversion were numerically investigated in terms of large eddy simulation.

59 In this paper, The nonlinear resonant evolution of a two-dimensional fundamental wave and a pair of three-dimensional oblique subharmonic waves in a laminar boundary layer has been studied.

60 Vertex boundary layer phenomena of solution of singularly perturbed boundary value problem for a kind of fourth order elliptic equation is studied in this paper.