Add to ORKGThe program presented is a contracted effort to evolve and demonstrate the technology required to ut...
It was experimentally determined that the liquid boric oxide particles leaving a jet engine combusto...
Concern over the future availability of high quality liquid fuels or use in furnaces and boilers pro...
Investigation on size and density of boric oxide exhaust cloud of turbojet engine operating on trime...
An experimental investigation was conducted on a centrifugal-type turbojet engine using a 50-50 mixt...
In aa e f fo r t t o provide a better understanding of the effect of oxide-depositing fuels on engin...
Effect of fuel injector and liner design on performance of turbojet combustor with vapor fue
A preliminary investigation was conducted to determine the combustion characteristics of a fuel comp...
This report presents methods by which it is possible to determine, in a simple manner, both pressure...
Boron and its hydrides offer increased flight range relative to conventional fuels for turbojet engi...
The tendency for the jet engine rotor to continue to rotate after crash presents the probability tha...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
Performance characteristics of four hydrocarbon fuels having high Btu per gallon were determined in ...
of Aeronautics, Department of the Navy, seeking a high-energy fuel suit-able for turbo jet-powered ...
The next generation of commercial aircraft will include turbofan engines with performance significan...
The program presented is a contracted effort to evolve and demonstrate the technology required to ut...
It was experimentally determined that the liquid boric oxide particles leaving a jet engine combusto...
Concern over the future availability of high quality liquid fuels or use in furnaces and boilers pro...
Investigation on size and density of boric oxide exhaust cloud of turbojet engine operating on trime...
An experimental investigation was conducted on a centrifugal-type turbojet engine using a 50-50 mixt...
In aa e f fo r t t o provide a better understanding of the effect of oxide-depositing fuels on engin...
Effect of fuel injector and liner design on performance of turbojet combustor with vapor fue
A preliminary investigation was conducted to determine the combustion characteristics of a fuel comp...
This report presents methods by which it is possible to determine, in a simple manner, both pressure...
Boron and its hydrides offer increased flight range relative to conventional fuels for turbojet engi...
The tendency for the jet engine rotor to continue to rotate after crash presents the probability tha...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
Performance characteristics of four hydrocarbon fuels having high Btu per gallon were determined in ...
of Aeronautics, Department of the Navy, seeking a high-energy fuel suit-able for turbo jet-powered ...
The next generation of commercial aircraft will include turbofan engines with performance significan...
The program presented is a contracted effort to evolve and demonstrate the technology required to ut...
It was experimentally determined that the liquid boric oxide particles leaving a jet engine combusto...
Concern over the future availability of high quality liquid fuels or use in furnaces and boilers pro...