A brief overview and technical highlights of the research efforts and studies on rotary engines over the last several years at the NASA Lewis Research Center are presented. The test results obtained from turbocharged rotary engines and preliminary results from a high performance single rotor engine were discussed. Combustion modeling studies of the rotary engine and the use of a Laser Doppler Velocimeter to confirm the studies were examined. An in-house program in which a turbocharged rotary engine was installed in a Cessna Skymaster for ground test studies was reviewed. Details are presented on single rotor stratified charge rotary engine research efforts, both in-house and on contract
NASA is conducting aeronautical research over a broad range of Mach numbers. In addition to the gene...
A parametric study was performed to determine the performance limits of a rotary combustion engine. ...
The Small Turboshaft Engine Research (STER) program provides a vehicle for evaluating the applicatio...
Design studies of advanced multifuel general aviation and commuter aircraft rotary stratified charge...
The performance of a turbocharged rotary engine at power levels above 75 kW (100 hp) was studied. A ...
This paper overviews the current program, whose objective is to establish the generic technology bas...
The state of development of the rotary combustion engine is discussed. The nonturbine engine researc...
This report summarizes results of a critical technology enablement effort with the stratified charge...
The performance of internal combustion stratified-charge engines is highly dependent on the in-cylin...
Performance, weight, size, and maintenance data for advanced rotary aircraft engines suitable for co...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
Small engine technology programs being conducted at the NASA Lewis Research Center are described. Sm...
The role of the Lewis Research Center in aeronautical propulsion is described. The state of the art ...
NASA is responsible for advancing technologies related to air transportation. A sampling of the work...
A technology base of new developments which offered potential benefits to a general aviation engine ...
NASA is conducting aeronautical research over a broad range of Mach numbers. In addition to the gene...
A parametric study was performed to determine the performance limits of a rotary combustion engine. ...
The Small Turboshaft Engine Research (STER) program provides a vehicle for evaluating the applicatio...
Design studies of advanced multifuel general aviation and commuter aircraft rotary stratified charge...
The performance of a turbocharged rotary engine at power levels above 75 kW (100 hp) was studied. A ...
This paper overviews the current program, whose objective is to establish the generic technology bas...
The state of development of the rotary combustion engine is discussed. The nonturbine engine researc...
This report summarizes results of a critical technology enablement effort with the stratified charge...
The performance of internal combustion stratified-charge engines is highly dependent on the in-cylin...
Performance, weight, size, and maintenance data for advanced rotary aircraft engines suitable for co...
A broad overview of the scope of research presently being supported by NASA in aircraft propulsion i...
Small engine technology programs being conducted at the NASA Lewis Research Center are described. Sm...
The role of the Lewis Research Center in aeronautical propulsion is described. The state of the art ...
NASA is responsible for advancing technologies related to air transportation. A sampling of the work...
A technology base of new developments which offered potential benefits to a general aviation engine ...
NASA is conducting aeronautical research over a broad range of Mach numbers. In addition to the gene...
A parametric study was performed to determine the performance limits of a rotary combustion engine. ...
The Small Turboshaft Engine Research (STER) program provides a vehicle for evaluating the applicatio...