Add to ORKGAfterburning turbojet, nonafterburning turbojet, and duct burning turbofan designs for supersonic transports with and without takeoff noise constraint
A concept is presented that combines the low-noise and high-thrust characteristics of a turbofan at ...
Parametric turbofan engine study for Mach 0.98 transport with low takeoff and approach noise levels ...
The effect of turbofan engine overall pressure ratio, fan pressure ratio, and ductburner temperature...
Influence of high turbine inlet temperature and take off jet noise on methane fueled supersonic tran...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
A parametric study was made of duct-burning turbofan and suppressed dry turbojet engines installed i...
Emissions of total oxides of nitrogen, nitric oxide, unburned hydrocarbons, carbon monoxide, and car...
A performance test of several experimental afterburner configurations was conducted with a mixed-flo...
N 69-14386.Includes bibliographical references (p. 56).Mode of access: Internet.System requirements:...
A study was conducted to determine the promising propulsion systems for advanced supersonic transpor...
A study was made of an advanced technology airplane using supercritical aerodynamics. Cruise Mach nu...
Every advance in the transformation of heat energy into mechanical energy has involved a noise probl...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
The continuing improvement of aircraft gas turbine engine operating efficiencies involves increases ...
For turbojet engines designed for flight Mach numbers of 2.5 and 3.0, use of turbine stator adjustme...
A concept is presented that combines the low-noise and high-thrust characteristics of a turbofan at ...
Parametric turbofan engine study for Mach 0.98 transport with low takeoff and approach noise levels ...
The effect of turbofan engine overall pressure ratio, fan pressure ratio, and ductburner temperature...
Influence of high turbine inlet temperature and take off jet noise on methane fueled supersonic tran...
Turbine aerodynamic and cooling requirements for turbojet powered Mach 3 transport using methane fue
A parametric study was made of duct-burning turbofan and suppressed dry turbojet engines installed i...
Emissions of total oxides of nitrogen, nitric oxide, unburned hydrocarbons, carbon monoxide, and car...
A performance test of several experimental afterburner configurations was conducted with a mixed-flo...
N 69-14386.Includes bibliographical references (p. 56).Mode of access: Internet.System requirements:...
A study was conducted to determine the promising propulsion systems for advanced supersonic transpor...
A study was made of an advanced technology airplane using supercritical aerodynamics. Cruise Mach nu...
Every advance in the transformation of heat energy into mechanical energy has involved a noise probl...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
The continuing improvement of aircraft gas turbine engine operating efficiencies involves increases ...
For turbojet engines designed for flight Mach numbers of 2.5 and 3.0, use of turbine stator adjustme...
A concept is presented that combines the low-noise and high-thrust characteristics of a turbofan at ...
Parametric turbofan engine study for Mach 0.98 transport with low takeoff and approach noise levels ...
The effect of turbofan engine overall pressure ratio, fan pressure ratio, and ductburner temperature...