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Author: SOLOMON. CIOLKOWSKI Publisher: ISBN: Category : Languages : en Pages : 1
Book Description
A study is presented of an ideal gas shock impinging on a wall. The flow produced by a shock moving in a tube with a constriction is analyzed. The analysis is then applied to the solution of the shock impingement on a constriction. The state of the gas produced by the interaction of a shock with a constriction is determined for the case where the shock is reflected. Contraction ratios are determined so that the shock is reflected. The interaction of a shock with an interface is studied and conditions are determined so that a reflected shock is not produced. In the last section methods are proposed which can be used to analyze the above situations for real gases in thermodynamic equilibrium. (Author).
Author: SOLOMON. CIOLKOWSKI Publisher: ISBN: Category : Languages : en Pages : 1
Book Description
A study is presented of an ideal gas shock impinging on a wall. The flow produced by a shock moving in a tube with a constriction is analyzed. The analysis is then applied to the solution of the shock impingement on a constriction. The state of the gas produced by the interaction of a shock with a constriction is determined for the case where the shock is reflected. Contraction ratios are determined so that the shock is reflected. The interaction of a shock with an interface is studied and conditions are determined so that a reflected shock is not produced. In the last section methods are proposed which can be used to analyze the above situations for real gases in thermodynamic equilibrium. (Author).
Author: W. B. JR. BROWER Publisher: ISBN: Category : Compressibility Languages : en Pages : 1
Book Description
Equations for the asymptotic flow due to passage of a shock through a constriction are presented. The region of ambiguity which involved 3 possible solutions with either a reflected shock, a standing shock, or no shock, is reviewed. A wave diagram is constructed to show that the solution involving no reflection is unstable under a small but finite disturbance. Kantrowitz's perturbation equations for non-steady, one-dimensional flow through a particular, non-uniform, nozzle are used to investigate the problem of shock formation due to expansion-disturbances. Two problems are considered: the first is a complete treatment of shock formation in a de Laval nozzle; the second is the case of shock formation in a decelerating supersonic flow. Results of the second case are then used to formulate a criterion for the stability of the solution for flow through a constriction without a reflected shock, under action of a small disturbance. (Author).
Author: John W. Wescott Publisher: ISBN: Category : Air Languages : en Pages : 650
Book Description
This bibliography contains several thousand abstracts from the unclassified literature on the propagation of sound in air. The subject is treated in depth for the years 1929 to 1963. Some abstracts on earlier works of lasting interest and many abstracts from English translations of foreign journals are included. The abstracts are grouped according to subject matter. Subject and author indexes are furnished. Accessions Document (AD and earlier ATI) numbers used by both the Defense Documentation Center (formerly ASTIA) and the Office of Technical Services (OTS) are furnished wherever possible. (Author).
Author: SOLOMON. CIOLKOWSKI
Author: SOLOMON. CIOLKOWSKI
Author: W. B. JR. BROWER
Author: William B. Brower
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Author: Louis G. Kaufman
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Author: Arnold M. Melnick
Author: John W. Wescott