Add to ORKGA study program for conceptual design studies of remote lift and lift/cruise fan systems to meet the requirements of military V/STOL aircraft was conducted. Parametric performance and design data are presented for fans covering a range of pressure ratios, including both single and two stage fan concepts. The gas generator selected for these fan systems was the J101-GE-100 engine. Noise generation and transient response were determined for selected fan systems
Technology flight vehicles were defined for three different approaches which demonstrate the concept...
Preliminary designs of three integral lift fan engines suitable for commercial certification in the ...
Additional preliminary design studies were performed for a turbotip lift/cruise fan propulsion syste...
Conceptual design studies of V/STOL Lift Fan Commercial short-haul transport aircraft for the 1980-8...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Two types of lift/cruise fan technology aircraft were conceptually designed. One aircraft used turbo...
Thermodynamic, aerodynamic, mechanical, and systems studies of lift fan concepts for V/STOL TRANSPOR...
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Aerodynamic characteristics of lift fan installation for direct lift V/STOL aircraf
Preliminary design studies were performed to define a turbotip lift/cruise fan propulsion system for...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
A three engine, three fan V/STOL airplane was designed for use as a Research Technology Airplane in ...
The initial design of the LCF459 lift/cruise fan system is documented. The LCF459 is a 1.5 meter dia...
Concept design is presented for two types of lift/cruise fan technology V/STOL aircraft, turbotip fa...
Technology flight vehicles were defined for three different approaches which demonstrate the concept...
Preliminary designs of three integral lift fan engines suitable for commercial certification in the ...
Additional preliminary design studies were performed for a turbotip lift/cruise fan propulsion syste...
Conceptual design studies of V/STOL Lift Fan Commercial short-haul transport aircraft for the 1980-8...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Two types of lift/cruise fan technology aircraft were conceptually designed. One aircraft used turbo...
Thermodynamic, aerodynamic, mechanical, and systems studies of lift fan concepts for V/STOL TRANSPOR...
A simplified mission analysis was performed to determine an optimum engine cycle for a 100-passenger...
Conceptual designs of V/STOL lift fan commercial short haul transport aircraft for the 1980-85 time ...
Aerodynamic characteristics of lift fan installation for direct lift V/STOL aircraf
Preliminary design studies were performed to define a turbotip lift/cruise fan propulsion system for...
A design study was conducted for a remote lift-fan commercial V/STOL transport for the 1985 time per...
A three engine, three fan V/STOL airplane was designed for use as a Research Technology Airplane in ...
The initial design of the LCF459 lift/cruise fan system is documented. The LCF459 is a 1.5 meter dia...
Concept design is presented for two types of lift/cruise fan technology V/STOL aircraft, turbotip fa...
Technology flight vehicles were defined for three different approaches which demonstrate the concept...
Preliminary designs of three integral lift fan engines suitable for commercial certification in the ...
Additional preliminary design studies were performed for a turbotip lift/cruise fan propulsion syste...