The Starting Process in a Hypersonic Nozzle

The Starting Process in a Hypersonic Nozzle PDF Author: C. Edward Smith
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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The Starting Process in a Hypersonic Nozzle

The Starting Process in a Hypersonic Nozzle PDF Author: C. Edward Smith
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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Book Description


An Analytic Study of the Starting Process in a Hypersonic Nozzle

An Analytic Study of the Starting Process in a Hypersonic Nozzle PDF Author: Charles Edward Smith
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 174

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Book Description


The Starting Process in a Hypersonic Nozzle

The Starting Process in a Hypersonic Nozzle PDF Author: C. Edward Smith
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

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Book Description


An Analytic Study of the Starting Process in a Hypersonic Nozzle

An Analytic Study of the Starting Process in a Hypersonic Nozzle PDF Author: Charles Edward Smith (Jr.)
Publisher:
ISBN:
Category : Jets
Languages : en
Pages : 130

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A Finite-difference Analysis of the Nozzle Starting Process in an Expansion Tunnel

A Finite-difference Analysis of the Nozzle Starting Process in an Expansion Tunnel PDF Author: K. James Weilmuenster
Publisher:
ISBN:
Category : Finite differences
Languages : en
Pages : 56

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 574

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Method for Calculation of the One-dimensional Nonequilibrium Flow of a General Gas Mixture Through a Hypersonic Nozzle

Method for Calculation of the One-dimensional Nonequilibrium Flow of a General Gas Mixture Through a Hypersonic Nozzle PDF Author: George Emanuel
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 112

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Book Description
The work described is a continuation of that reported previously in AEDC-TN-61-65 (calculation of the one-dimensional nonequilibrium flow of air through a hypersonic nozzle). In particular, a method is presented for the exact numerical calculation of the one-dimensional nonequilibrium flow of a general gas mixture through a converging-diverging nozzle. General equations are given for a mixture of perfect gases with an arbitrary number of species undergoing an arbitrary number of chemical and vibrational rate processes. An inexact but accurate method, similar in form to the method employed in the nonequilibrium case, is also given for calculating the corresponding one-dimensional equilibrium flow. The numerical method of solution applicable to both cases is described, including a simple procedure for starting the nonequilibrium calculations from an equilibrium condition and an improved method for controlling integration step size. The factors that affect over-all computation time are discussed. A computer program for an IBM 7090 has been written for the general gas mixture. Specific calculations are reported for a model of air consisting of O, N, NO, N2, and O2 and including eight chemical reactions plus the vibrational processes of the three diatomic species.

Shock Waves

Shock Waves PDF Author: Klaus Hannemann
Publisher: Springer Science & Business Media
ISBN: 354085181X
Category : Science
Languages : en
Pages : 786

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Book Description
The 26th International Symposium on Shock Waves in Göttingen, Germany was jointly organised by the German Aerospace Centre DLR and the French-German Research Institute of Saint Louis ISL. The year 2007 marked the 50th anniversary of the Symposium, which first took place in 1957 in Boston and has since become an internationally acclaimed series of meetings for the wider Shock Wave Community. The ISSW26 focused on the following areas: Shock Propagation and Reflection, Detonation and Combustion, Hypersonic Flow, Shock Boundary Layer Interaction, Numerical Methods, Medical, Biological and Industrial Applications, Richtmyer Meshkov Instability, Blast Waves, Chemically Reacting Flows, Diagnostics, Facilities, Flow Visualisation, Ignition, Impact and Compaction, Multiphase Flow, Nozzles Flows, Plasmas and Propulsion. The two Volumes contain the papers presented at the symposium and serve as a reference for the participants of the ISSW 26 and individuals interested in these fields.

Experimental Study of the Starting Process, Flow Duration, and Nozzle Boundary Layer in a High-enthalpy Shock Tunnel

Experimental Study of the Starting Process, Flow Duration, and Nozzle Boundary Layer in a High-enthalpy Shock Tunnel PDF Author: Michael G. Dunn
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 92

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Design of an Axisymmetric, Hypersonic Nozzle, Utilizing the Method of Characteristics

Design of an Axisymmetric, Hypersonic Nozzle, Utilizing the Method of Characteristics PDF Author: Vincent Patrick Bailey
Publisher:
ISBN:
Category : Supersonic nozzles
Languages : en
Pages : 124

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