Author: Richard Frank Hoglund
Publisher:
ISBN:
Category : Boundary layer. 650
Languages : en
Pages : 282
Book Description
The boundary layer approximation is applied to the equations governing the mixing zone between two parallel semi-infinite streams. The two streams differ in composition and temperature, but they are not necessarily in chemical equilibrium. Closed form solutions are obtained for the approach to equilibrium in the mixing zone in the case of equal velocitiesof the two streams. Frozen flow and equilibrium flow appear as limiting cases of the general solution. A linearized reaction rate law is used for the no-equilibrium stituations. These solutions indicate that the major factor contributing to non-equilibrium conditions outside of the mixing zone is the presence of non-equilibrium conditions outside of the mixing zone. An approximate solution to the case of unequal free stream velocities is obtained using an equilibrium condition found to be applicable in the constant velocity case. The results of these studies are used to provide a qualitative indication of the effects of dissociation and ionization reactions on the flow field immediately behind a hypersonic body. It is found that the presence of reactions in various regions of this flow field causes individual and discernible changes in the wake expansion angle and in the base pressure.
Dissociation and ionization effects in the laminar mixing of parallel streams
Author: Richard Frank Hoglund
Publisher:
ISBN:
Category : Boundary layer. 650
Languages : en
Pages : 282
Book Description
The boundary layer approximation is applied to the equations governing the mixing zone between two parallel semi-infinite streams. The two streams differ in composition and temperature, but they are not necessarily in chemical equilibrium. Closed form solutions are obtained for the approach to equilibrium in the mixing zone in the case of equal velocitiesof the two streams. Frozen flow and equilibrium flow appear as limiting cases of the general solution. A linearized reaction rate law is used for the no-equilibrium stituations. These solutions indicate that the major factor contributing to non-equilibrium conditions outside of the mixing zone is the presence of non-equilibrium conditions outside of the mixing zone. An approximate solution to the case of unequal free stream velocities is obtained using an equilibrium condition found to be applicable in the constant velocity case. The results of these studies are used to provide a qualitative indication of the effects of dissociation and ionization reactions on the flow field immediately behind a hypersonic body. It is found that the presence of reactions in various regions of this flow field causes individual and discernible changes in the wake expansion angle and in the base pressure.
Publisher:
ISBN:
Category : Boundary layer. 650
Languages : en
Pages : 282
Book Description
The boundary layer approximation is applied to the equations governing the mixing zone between two parallel semi-infinite streams. The two streams differ in composition and temperature, but they are not necessarily in chemical equilibrium. Closed form solutions are obtained for the approach to equilibrium in the mixing zone in the case of equal velocitiesof the two streams. Frozen flow and equilibrium flow appear as limiting cases of the general solution. A linearized reaction rate law is used for the no-equilibrium stituations. These solutions indicate that the major factor contributing to non-equilibrium conditions outside of the mixing zone is the presence of non-equilibrium conditions outside of the mixing zone. An approximate solution to the case of unequal free stream velocities is obtained using an equilibrium condition found to be applicable in the constant velocity case. The results of these studies are used to provide a qualitative indication of the effects of dissociation and ionization reactions on the flow field immediately behind a hypersonic body. It is found that the presence of reactions in various regions of this flow field causes individual and discernible changes in the wake expansion angle and in the base pressure.
U.S. Government Research Reports
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 950
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 950
Book Description
Journal of the Royal Aeronautical Society
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 946
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 946
Book Description
The Journal of the Royal Aeronautical Society
Author: Royal Aeronautical Society
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1156
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1156
Book Description
International Aerospace Abstracts
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1064
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1064
Book Description
Journal of the Aero/space Sciences
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1550
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1550
Book Description
The Journal of the Royal Aeronautical Society
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 600
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 600
Book Description
Report
Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 844
Book Description
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 844
Book Description
Hydraulic Research in the United States
Author:
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 230
Book Description
Publisher:
ISBN:
Category : Hydraulic engineering
Languages : en
Pages : 230
Book Description
Miscellaneous Publication - National Bureau of Standards
Author: United States. National Bureau of Standards
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 238
Book Description
Publisher:
ISBN:
Category : Weights and measures
Languages : en
Pages : 238
Book Description