Author: Laurence N. Connor (Jr.)
Publisher:
ISBN:
Category : Enthalpy
Languages : en
Pages : 50
Book Description
Calculation of the Centered One-dimensional Unsteady Expansion of a Reacting Gas Mixture Subject to Vibrational and Chemical Nonequilibrium
Author: Laurence N. Connor (Jr.)
Publisher:
ISBN:
Category : Enthalpy
Languages : en
Pages : 50
Book Description
Publisher:
ISBN:
Category : Enthalpy
Languages : en
Pages : 50
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
NASA Technical Note
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 572
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 572
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 428
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 428
Book Description
A Selected Listing of NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 436
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 436
Book Description
Reaction Rates for High-temperature Air with Carbon and Sodium Impurities
Author: Mina L. Carnicom
Publisher:
ISBN:
Category : Gases at high temperatures
Languages : en
Pages : 156
Book Description
The values used by a number of investigators for the rate constants of high-temperature ([greater than or equal to]1000©K) homogeneous gaseous reactions involving species of the elements nitrogen, oxygen, carbon, and sodium have been compiled and are presented in tabular form. Included are reactions involving neutral species, charged species, free electrons, some species in excited electronic or vibrational states, and radiative processes.
Publisher:
ISBN:
Category : Gases at high temperatures
Languages : en
Pages : 156
Book Description
The values used by a number of investigators for the rate constants of high-temperature ([greater than or equal to]1000©K) homogeneous gaseous reactions involving species of the elements nitrogen, oxygen, carbon, and sodium have been compiled and are presented in tabular form. Included are reactions involving neutral species, charged species, free electrons, some species in excited electronic or vibrational states, and radiative processes.
SCR.
Author:
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 156
Book Description
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 156
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 688
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 688
Book Description
Government-wide Index to Federal Research & Development Reports
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1078
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1078
Book Description
Free-stream Temperature, Density, and Pressure Measurements in an Expansion Tube Flow
Author: Kenneth V. Haggard
Publisher:
ISBN:
Category : Expansion tubes (Hypersonic wind tunnels)
Languages : en
Pages : 60
Book Description
An experimental study was conducted to determine test-flow conditions in the Langley pilot model expansion tube. Measurements of temperature, density, wall pressure, pitot pressure, and shock and interface velocities were compared with theoretical calculations based on various models of the flow cycle. The vibrational temperature and integrated density of the molecular oxygen component of the flow were measured by use of vacuum ultraviolet absorption techniques. These measurements indicate both the presence and possible degree of nonequilibrium in the flow. Data are compared with several simplified models of the flow cycle, and data trends are discussed.
Publisher:
ISBN:
Category : Expansion tubes (Hypersonic wind tunnels)
Languages : en
Pages : 60
Book Description
An experimental study was conducted to determine test-flow conditions in the Langley pilot model expansion tube. Measurements of temperature, density, wall pressure, pitot pressure, and shock and interface velocities were compared with theoretical calculations based on various models of the flow cycle. The vibrational temperature and integrated density of the molecular oxygen component of the flow were measured by use of vacuum ultraviolet absorption techniques. These measurements indicate both the presence and possible degree of nonequilibrium in the flow. Data are compared with several simplified models of the flow cycle, and data trends are discussed.