Author: Thomas P. MoffittPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 34
Book Description
Design and Experimental Investigation of a Single-stage Turbine with a Rotor Entering Relative Mach Number of 2
Author: Thomas P. MoffittPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 34
Book Description
Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine
Author: Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine
Author: Thomas P. MoffittPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 20
Book Description
Design and Experimental Investigation of Two Rotor Blade Modifications for a High-weight-flow Low-pressure-ratio Turbine
Author: Robert R. NunamakerPublisher:
ISBN:
Category : Turbines
Languages : en
Pages : 30
Book Description
Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine
Author: Thomas P. MoffittPublisher:
ISBN:
Category : Turbines
Languages : en
Pages : 26
Book Description
Turbine Design and Application
Author: Arthur J. GlassmanPublisher:
ISBN:
Category : Aircraft gas-turbines
Languages : en
Pages : 152
Book Description
NASA Technical Note
Author: U.S. Government Research Reports
Author: Experimental Investigation of a 3.0-inch-mean-diameter Full-admission Three-stage Turbine Suitable for Small Auxiliary Power Units
Author: Robert Young WongPublisher:
ISBN:
Category : Gas-turbines
Languages : en
Pages : 26
Book Description
Author: