A computer program has been written that performs the flow parameter calculations for cryogenic wind tunnels which use nitrogen as a test gas. The flow parameters calculated include static pressure, static temperature, compressibility factor, ratio of specific heats, dynamic viscosity, total and static density, velocity, dynamic pressure, mass-flow rate, and Reynolds number. Simplifying assumptions have been made so that the calculations of Reynolds number, as well as the other flow parameters can be made on relatively small desktop digital computers. The program, which also includes various power calculations, has been developed to the point where it has become a very useful tool for the users and possible future designers of fan-driven co...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The design and performance of a low speed one atmosphere cryogenic wind tunnel is described. The tun...
In order to evaluate hot jet simulation capability in cryogenic wind tunnel testing, simple theoreti...
The cryogenic concept and the advantages it offers with respect to achieving full scale Reynolds num...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
A theoretical analysis has been made of the power required for isentropic compressions of cryogenic ...
The design of a cryogenic wind tunnel which operates continuously, and is capable of attaining trans...
The National Transonic Facility (NTF), a fan-driven, transonic, pressurized, cryogenic wind tunnel, ...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
The minimum operating temperature which avoids real-gas effects, such as condensation, was determine...
A theoretical analysis was made of the power required for isentropic compressions of cryogenic nitro...
Computer program obtains the real-gas isentropic flow functions and thermodynamic properties of gase...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
A method of reliquefying from 12 to 19% of the nitrogen exhaust gas from a cryogenic wind tunnel has...
Cold wire measurement of temperature fluctuations were made in a DERAT T'2 induction powered cryogen...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The design and performance of a low speed one atmosphere cryogenic wind tunnel is described. The tun...
In order to evaluate hot jet simulation capability in cryogenic wind tunnel testing, simple theoreti...
The cryogenic concept and the advantages it offers with respect to achieving full scale Reynolds num...
Experiments performed at the NASA Langley Research Center in a cryogenic low-speed continuous-flow t...
A theoretical analysis has been made of the power required for isentropic compressions of cryogenic ...
The design of a cryogenic wind tunnel which operates continuously, and is capable of attaining trans...
The National Transonic Facility (NTF), a fan-driven, transonic, pressurized, cryogenic wind tunnel, ...
The cryogenic wind-tunnel concept as a practical means for improving ground simulation of transonic ...
The minimum operating temperature which avoids real-gas effects, such as condensation, was determine...
A theoretical analysis was made of the power required for isentropic compressions of cryogenic nitro...
Computer program obtains the real-gas isentropic flow functions and thermodynamic properties of gase...
A representative, control compatible, mathematical model of a cryogenic wind tunnel was synthesized ...
A method of reliquefying from 12 to 19% of the nitrogen exhaust gas from a cryogenic wind tunnel has...
Cold wire measurement of temperature fluctuations were made in a DERAT T'2 induction powered cryogen...
The results of the cryogenic wind tunnel program conducted at NASA Langley Research Center are prese...
The design and performance of a low speed one atmosphere cryogenic wind tunnel is described. The tun...
In order to evaluate hot jet simulation capability in cryogenic wind tunnel testing, simple theoreti...