Add to ORKGCost estimations, noise constraints, and supercritical wing compatibility in optimization of turbofan engines for Mach 0.90 to Mach 0.98 commercial air transport
Full-scale low-tip-speed fans, a full-scale high-tip-speed fan, scale model versions of fans, and tw...
A study was made of the effects of turbofan cycle parameters and the use of acoustic noise suppressi...
The optimum design of nacelles that operate over a wide range of aerodynamic conditions and their in...
Parametric turbofan engine study for Mach 0.98 transport with low takeoff and approach noise levels ...
A study was made of an advanced technology airplane using supercritical aerodynamics. Cruise Mach nu...
The procedures that are used to select engines for transport and combat aircraft are discussed. In g...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
Modern high speed propeller (advanced turboprop) aircraft are expected to operate on 50 to 60 percen...
The effect of turbofan engine overall pressure ratio, fan pressure ratio, and ductburner temperature...
Results are presented of NASA studies to determine optimum engine cycles for noise levels of 10, 15,...
The results of four years research on technology are synthesized in an advanced supersonic cruise ai...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
Parametric engine study for Mach 0.98 commercial air transport with supercritical win
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
Engine performance and mission studies were performed for turbofan engines with supersonic through-f...
Full-scale low-tip-speed fans, a full-scale high-tip-speed fan, scale model versions of fans, and tw...
A study was made of the effects of turbofan cycle parameters and the use of acoustic noise suppressi...
The optimum design of nacelles that operate over a wide range of aerodynamic conditions and their in...
Parametric turbofan engine study for Mach 0.98 transport with low takeoff and approach noise levels ...
A study was made of an advanced technology airplane using supercritical aerodynamics. Cruise Mach nu...
The procedures that are used to select engines for transport and combat aircraft are discussed. In g...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
Modern high speed propeller (advanced turboprop) aircraft are expected to operate on 50 to 60 percen...
The effect of turbofan engine overall pressure ratio, fan pressure ratio, and ductburner temperature...
Results are presented of NASA studies to determine optimum engine cycles for noise levels of 10, 15,...
The results of four years research on technology are synthesized in an advanced supersonic cruise ai...
The need for greatly improved fuel efficiency and off-design subsonic characteristics is discussed. ...
Parametric engine study for Mach 0.98 commercial air transport with supercritical win
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
Engine performance and mission studies were performed for turbofan engines with supersonic through-f...
Full-scale low-tip-speed fans, a full-scale high-tip-speed fan, scale model versions of fans, and tw...
A study was made of the effects of turbofan cycle parameters and the use of acoustic noise suppressi...
The optimum design of nacelles that operate over a wide range of aerodynamic conditions and their in...