The Sonic Throat Method And Real Gas One Dimensional Flow An Application To Air And Nitrogen
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Author | : Richard L. Humphrey |
Publisher | : |
Total Pages | : 52 |
Release | : 1971 |
Genre | : Hypersonic wind tunnels |
ISBN | : |
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).
Author | : Richard L. Humphrey |
Publisher | : |
Total Pages | : 30 |
Release | : 1971 |
Genre | : |
ISBN | : |
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).
Author | : |
Publisher | : |
Total Pages | : 488 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
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.
Author | : John David Anderson (Jr.) |
Publisher | : |
Total Pages | : 80 |
Release | : 1971 |
Genre | : Expansion of gases |
ISBN | : |
It is well established that population inversions between the (001) and (100) vibrational energy levels of CO2 can be created by rapid expansions of CO2-N2-H2O or He mixtures through supersonic nozzles. New experimental results are presented for such inversions. These experiments were conducted in both the 3-Megawatt Arc Tunnel and the 12.7 cm Shock Tunnel at the Naval Ordnance Laboratory. The results support previously published theoretical predictions obtained with a numerical, time-dependent, nonequilibrium nozzle flow analysis employing a simplified vibrational kinetic model. This theory is also compared with experimental data obtained by other investigators. (Author).
Author | : Allen F. Donovan |
Publisher | : Princeton University Press |
Total Pages | : 1021 |
Release | : 2015-12-08 |
Genre | : Science |
ISBN | : 140087503X |
Volume VIII of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: performance calculation at high speed; stability and control of high speed aircraft; aeroelasticity and flutter; model testing; transonic wind tunnels; supersonic tunnels; hypersonic experimental facilities; low density wind tunnels; shock tube; wind tunnel measurements; instrumented models in free flight; piloted aircraft testing; free flight range methods. Originally published in 1961. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author | : |
Publisher | : |
Total Pages | : 314 |
Release | : 1974 |
Genre | : Mechanical engineering |
ISBN | : |
Author | : John E. Grimaud |
Publisher | : |
Total Pages | : 40 |
Release | : 1964 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 656 |
Release | : 1964 |
Genre | : |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 568 |
Release | : 1973 |
Genre | : Mechanics, Applied |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1076 |
Release | : 1982 |
Genre | : Aeronautics |
ISBN | : |