The NASA Advanced Aviation Comparative Engine/Airframe Integration Study was initiated to help determine which of four promising concepts for new general aviation engines for the 1990's should be considered for further research funding. The engine concepts included rotary, diesel, spark ignition, and turboprop powerplants; a conventional state-of-the-art piston engine was used as a baseline for the comparison. Computer simulations of the performance of single and twin engine pressurized aircraft designs were used to determine how the various characteristics of each engine interacted in the design process. Comparisons were made of how each engine performed relative to the others when integrated into an airframe and required to fly a transpor...
Propulsion system technologies applicable to the generation of commuter airline aircraft expected to...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The research objectives of the NASA aircraft energy efficiency program are summarized. Engine compon...
A comparison of the in-airframe performance and efficiency of the advanced engine concepts is presen...
An investigation was conducted to identify candidate technologies and specific developments which of...
The small engine technology requirements suitable for general aviation service in the 1987 to 1988 t...
The application of advanced control concepts to air breathing engines may yield significant improvem...
Design studies of advanced multifuel general aviation and commuter aircraft rotary stratified charge...
A technology base of new developments which offered potential benefits to a general aviation engine ...
A study was made to examine the effect of advanced technology engines on the performance of subsonic...
The feasibility of turbine engines for the smaller general aviation aircraft was investigated and a ...
Definitions of takeoff gross weight, performance, and direct operating cost for both a 30 and 50 pas...
Results of aircraft/engine integration studies conducted on an advanced flight propulsion system are...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
Engine/airframe compatibilities are studied utilizing the advanced supersonic transport point design...
Propulsion system technologies applicable to the generation of commuter airline aircraft expected to...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The research objectives of the NASA aircraft energy efficiency program are summarized. Engine compon...
A comparison of the in-airframe performance and efficiency of the advanced engine concepts is presen...
An investigation was conducted to identify candidate technologies and specific developments which of...
The small engine technology requirements suitable for general aviation service in the 1987 to 1988 t...
The application of advanced control concepts to air breathing engines may yield significant improvem...
Design studies of advanced multifuel general aviation and commuter aircraft rotary stratified charge...
A technology base of new developments which offered potential benefits to a general aviation engine ...
A study was made to examine the effect of advanced technology engines on the performance of subsonic...
The feasibility of turbine engines for the smaller general aviation aircraft was investigated and a ...
Definitions of takeoff gross weight, performance, and direct operating cost for both a 30 and 50 pas...
Results of aircraft/engine integration studies conducted on an advanced flight propulsion system are...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
Engine/airframe compatibilities are studied utilizing the advanced supersonic transport point design...
Propulsion system technologies applicable to the generation of commuter airline aircraft expected to...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The research objectives of the NASA aircraft energy efficiency program are summarized. Engine compon...