Author: C. C. Limbaugh
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Calculations of Air Chemistry in the Electron-beam Heated Hypersonic Wind Tunnel
Author: C. C. Limbaugh
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Calculations of Air Chemicstry in the Electron-beam Heated Hypersonic Wind Tunnel II. Current Experiments
Author: C. C. Limbaugh
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
A Summary of Similitude Studies for High Enthalpy Hypersonic Test Facilities
Author: S. L. Petrie
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 40
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 384
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 384
Book Description
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1032
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1032
Book Description
The High Temperature Aspects of Hypersonic Flow
Author: Wilbur C. Nelson
Publisher: Elsevier
ISBN: 1483223310
Category : Science
Languages : en
Pages : 801
Book Description
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
Publisher: Elsevier
ISBN: 1483223310
Category : Science
Languages : en
Pages : 801
Book Description
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
Chemical Kinetic Regimes of Hypersonic Flight Simulation
Author: Donald J. Harney
Publisher:
ISBN:
Category : Chemical kinetics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Chemical kinetics
Languages : en
Pages : 32
Book Description
22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference: 02-2700 - 02-2926
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 694
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 694
Book Description
A Study of Equilibrium Real-gas Effects in Hypersonic Air Nozzles, Including Charts of Thermodynamic Properties for Equilibrium Air
Author: Wayne Douglas Erickson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 190
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 190
Book Description
The Sonic Throat Method and Real Gas One-dimensional Flow
Author: Richard L. Humphrey
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
Book Description
The one-dimensional flow equation for mass flow through the throat of a supersonic nozzle has been modified for use with real gas values of gamma and compressibility. Curve fits for gamma and Z and a simple iteration scheme have been developed for use with air and nitrogen over a temperature range of 300 to 6000 deg. K and a pressure of 10 to 100 atm. With this approach the sonic throat method can be used with the most recent gas tables to determine high temperature wind tunnel supply temperatures or enthalpies. (Author).
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
Book Description
The one-dimensional flow equation for mass flow through the throat of a supersonic nozzle has been modified for use with real gas values of gamma and compressibility. Curve fits for gamma and Z and a simple iteration scheme have been developed for use with air and nitrogen over a temperature range of 300 to 6000 deg. K and a pressure of 10 to 100 atm. With this approach the sonic throat method can be used with the most recent gas tables to determine high temperature wind tunnel supply temperatures or enthalpies. (Author).