Computations of Three-Dimensional Unsteady Supersonic Cavity Flow to Study the Effect of Different Downstream Geometries PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Computations of Three-Dimensional Unsteady Supersonic Cavity Flow to Study the Effect of Different Downstream Geometries PDF full book. Access full book title Computations of Three-Dimensional Unsteady Supersonic Cavity Flow to Study the Effect of Different Downstream Geometries by B. I. Soemarwoto. Download full books in PDF and EPUB format.
Author: B. I. Soemarwoto
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Get Book Here
Book Description
Computations of three-dimensional unsteady supersonic cavity flow are performed for a free-stream Mach number of 1.2. Two cavity geometries are considered: (i) a simple rectangular cavity of length-to-depth (L/D) and length-to-width (L/W) ratios of 4.5, and (ii) a cavity with a 450 ramp attached to the downstream wall of the simple rectangular cavity. Two flow models for computing the cavity flow field are assessed: (a) the Reynolds-Averaged Navier-Stokes (RANS) equations with a kappa-omega- turbulence model for the whole flow field, and (b) a combination of an inviscid flow model using the Euler equations for the domain outside the boundary layer and the RANS model for the boundary layer. The structures of the flow fields resulting from the different models are observed. The effect of the different downstream geometries is assessed.
Author: B. I. Soemarwoto
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Get Book Here
Book Description
Computations of three-dimensional unsteady supersonic cavity flow are performed for a free-stream Mach number of 1.2. Two cavity geometries are considered: (i) a simple rectangular cavity of length-to-depth (L/D) and length-to-width (L/W) ratios of 4.5, and (ii) a cavity with a 450 ramp attached to the downstream wall of the simple rectangular cavity. Two flow models for computing the cavity flow field are assessed: (a) the Reynolds-Averaged Navier-Stokes (RANS) equations with a kappa-omega- turbulence model for the whole flow field, and (b) a combination of an inviscid flow model using the Euler equations for the domain outside the boundary layer and the RANS model for the boundary layer. The structures of the flow fields resulting from the different models are observed. The effect of the different downstream geometries is assessed.
Author: B. I. Soemarwoto
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: B. I. Soemarwoto
Publisher:
ISBN:
Category :
Languages : en
Pages : 13
Get Book Here
Book Description
Author: Peter W. Duck
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Get Book Here
Book Description
The interaction between a shock wave (attached to a wedge) and small amplitude, three-dimensional disturbances of a uniform, supersonic, freestream flow are investigated. The paper extends the two-dimensional study of Duck et al(1), through the use of vector potentials, which render the problem tractable by the same techniques as in the two-dimensional case, in particular by expansion of the solution by means of a Fourier-Bessel series, in appropriately chosen coordinates. Results are presented for specific classes of freestream disturbances, and the study shows conclusively that the shock is stable to all classes of disturbances (i.e. time periodic perturbations to the shock do not grow downstream), provided the flow downstream of the shock is supersonic (loosely corresponding to the weak shock solution). This is shown from our numerical results and also by asymptotic analysis of the Fourier-Bessel series, valid far downstream of the shock.
Author: Chong-Wei Chu
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92
Get Book Here
Book Description
Author: Chong-Wei Chu
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 216
Get Book Here
Book Description
Author: Adriana Nastase
Publisher: Elsevier
ISBN: 008055699X
Category : Technology & Engineering
Languages : en
Pages : 425
Get Book Here
Book Description
Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. - Computational work and experimental results show the real-world application of computational results - Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations - Includes a fully optimized and integrated design for a proposed supersonic transport aircraft
Author: Douglas W. Dusing
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 592
Get Book Here
Book Description
