Add to ORKGUnsteady blade surface pressure data for the Large-Scale Advanced Prop-Fan (LAP) blade operation with angular inflow, wake inflow and uniform flow over a range of inflow Mach numbers of 0.02 to 0.70 is provided. The data are presented as Fourier coefficients for the first 35 harmonics of shaft rotational frequency. Also presented is a brief discussion of the unsteady blade response observed at takeoff and cruise conditions with angular and wake inflow
The effects of angle of attack of a propfan on the blade loading and details of the flow field by so...
During the past decade, aircraft engine manufacturers and scientists at NASA have worked on extendin...
Miniature pressure transducers were used to measure the fluctuating pressure on the fan blades of a ...
The aerodynamic pressure distribution was determined on a rotating Prop-Fan blade at the S1-MA wind ...
An experiment was performed by Hamilton Standard, Division of United Technologies Corporation, under...
The unsteady blade surface pressures were measured on the SR-7A propeller. The freestream Mach no., ...
The unsteady flowfield of a propfan operation at takeoff conditions with angular inflow is examined ...
A major source of the noise generated by high bypass ratio aircraft fan engines is the unsteady pres...
Unsteady blade surface pressures were measured on an advanced, highly swept propeller known as SR-3....
The unsteady blade pressures due to the operation of the propfan at an angle to the direction of the...
An unsteady 3-D Euler analysis technique is employed to compute the flow field of an advanced propel...
A single rotation model propeller (SR-7A) was tested at simulated takeoff/approach conditions (Mach ...
The effect of compressibility on unsteady blade pressures is studied by solving the three-dimensiona...
Discussed is Static Rotor Testing of the SR-7L Large Scale Advanced Prop-Fan (LAP). The LAP is an ad...
Abstract An experimental investigation of the aerodynamic response of the rotor blading of a single ...
The effects of angle of attack of a propfan on the blade loading and details of the flow field by so...
During the past decade, aircraft engine manufacturers and scientists at NASA have worked on extendin...
Miniature pressure transducers were used to measure the fluctuating pressure on the fan blades of a ...
The aerodynamic pressure distribution was determined on a rotating Prop-Fan blade at the S1-MA wind ...
An experiment was performed by Hamilton Standard, Division of United Technologies Corporation, under...
The unsteady blade surface pressures were measured on the SR-7A propeller. The freestream Mach no., ...
The unsteady flowfield of a propfan operation at takeoff conditions with angular inflow is examined ...
A major source of the noise generated by high bypass ratio aircraft fan engines is the unsteady pres...
Unsteady blade surface pressures were measured on an advanced, highly swept propeller known as SR-3....
The unsteady blade pressures due to the operation of the propfan at an angle to the direction of the...
An unsteady 3-D Euler analysis technique is employed to compute the flow field of an advanced propel...
A single rotation model propeller (SR-7A) was tested at simulated takeoff/approach conditions (Mach ...
The effect of compressibility on unsteady blade pressures is studied by solving the three-dimensiona...
Discussed is Static Rotor Testing of the SR-7L Large Scale Advanced Prop-Fan (LAP). The LAP is an ad...
Abstract An experimental investigation of the aerodynamic response of the rotor blading of a single ...
The effects of angle of attack of a propfan on the blade loading and details of the flow field by so...
During the past decade, aircraft engine manufacturers and scientists at NASA have worked on extendin...
Miniature pressure transducers were used to measure the fluctuating pressure on the fan blades of a ...