of Aeronautics, Department of the Navy, seeking a high-energy fuel suit-able for turbo jet-powered aircraft. ThFs work includes the?. " and com-bustion properties, experiments w L t h combustors designed to use baron cowounds, evaluation of boron fuels in fu l l- sca le tu rbo jets with and conibustion of pentaborane has been demonstrated i n a turbojet, an a f t e r-sumption have generally been obtained. Total running times have been quite brief. 7 " without afterburners, and ram-jet flights on boron fuels. Satisfactory 2 burner, and a ram jet. The anticipated reductions in specific fuel con-U The intention of t h i s r epor t I s t o review NACA par t ic ipa t ion in PrUJect Zip, a Bureau of Aeronautics, Department of th...
The search for environmentally sound, socially responsible, and economically viable renewable fuel g...
This report summarizes the full-scale engine tests of pentaborane, pentaborane - JP-4 fuel mixtures,...
An analytical investigation of the effects of fuel density and heating value on the cruising range o...
A preliminary investigation was conducted to determine the combustion characteristics of a fuel comp...
A full-scale turbojet engine was operated with pentaborane fuel continuously for 22 minutes at condi...
A ramjet engine is an attractive means of propulsion because of its high efficiency and simplicity. ...
Technologies are reviewed for improving the thermal stability of jet fuels, with reference to the ov...
The combustion character is t ics of several pentaborane- JP-4 (MIL-F-5624A) f u e l blends in a tur...
In aa e f fo r t t o provide a better understanding of the effect of oxide-depositing fuels on engin...
Design techniques and problems in combustors of turbojet engines operating on boron-containing fuel
Performance characteristics of four hydrocarbon fuels having high Btu per gallon were determined in ...
Surrogate fuels are mixtures of pure hydrocarbons that mimic specific properties of a real fuel. The...
The present work focuses on the possibility of combining the advantages of ramjet propulsion with th...
An experimental investigation was conducted on a centrifugal-type turbojet engine using a 50-50 mixt...
An extensive program was conducted to investigate the use of concentrated slurries of boron and magn...
The search for environmentally sound, socially responsible, and economically viable renewable fuel g...
This report summarizes the full-scale engine tests of pentaborane, pentaborane - JP-4 fuel mixtures,...
An analytical investigation of the effects of fuel density and heating value on the cruising range o...
A preliminary investigation was conducted to determine the combustion characteristics of a fuel comp...
A full-scale turbojet engine was operated with pentaborane fuel continuously for 22 minutes at condi...
A ramjet engine is an attractive means of propulsion because of its high efficiency and simplicity. ...
Technologies are reviewed for improving the thermal stability of jet fuels, with reference to the ov...
The combustion character is t ics of several pentaborane- JP-4 (MIL-F-5624A) f u e l blends in a tur...
In aa e f fo r t t o provide a better understanding of the effect of oxide-depositing fuels on engin...
Design techniques and problems in combustors of turbojet engines operating on boron-containing fuel
Performance characteristics of four hydrocarbon fuels having high Btu per gallon were determined in ...
Surrogate fuels are mixtures of pure hydrocarbons that mimic specific properties of a real fuel. The...
The present work focuses on the possibility of combining the advantages of ramjet propulsion with th...
An experimental investigation was conducted on a centrifugal-type turbojet engine using a 50-50 mixt...
An extensive program was conducted to investigate the use of concentrated slurries of boron and magn...
The search for environmentally sound, socially responsible, and economically viable renewable fuel g...
This report summarizes the full-scale engine tests of pentaborane, pentaborane - JP-4 fuel mixtures,...
An analytical investigation of the effects of fuel density and heating value on the cruising range o...