Zobrazeno 1 - 10
of 14
pro vyhledávání: '"JOSEPH V. FOA"'
Autor:
JOSEPH V. FOA, BERNARD M. LEADON
Publikováno v:
Journal of the Aeronautical Sciences. 11:329-338
Existing methods devised to simplify the tedious classic procedure of performance computation depend either upon generalized parameters or upon approximate curves valid only in a restricted range, with the result tha t calculations usually are not ac
Autor:
Joseph V. Foa
Publikováno v:
Journal of the Aeronautical Sciences. 9:523-528
The conditions for static longitudinal stability and controllability and for safety against stall of a canard-type airplane are investigated. I t is found that the designer's freedom of initiative in proportioning a canard is restricted in very defin
Autor:
Joseph V. Foa
Publikováno v:
Journal of Fluids Engineering. 95:513-518
The mechanism of cryptosteady-flow energy separation is described and analyzed in its most general form, with full consideration of the effects of bearing friction or other rotor torque, and of such asymmetries as unequal discharge pressures, periphe
Autor:
Joseph V. Foa, George Rudinger
Publikováno v:
Journal of the Aeronautical Sciences. 16:84-94
I t is shown that, contrary to widely accepted opinions: (a) The addition of heat to a subsonic flow in a pipe modifies the flow conditions both downstream and upstream of the region of heat addition. (b) The Mach Number of the heated flow does not n
Autor:
Joseph V. Foa
Publikováno v:
SAE Technical Paper Series.
Autor:
Joseph V. Foa
Publikováno v:
Journal of Aircraft. 18:500-501
Joseph V.Foa* The George Washington University, Washington, D.C. cascade of vanes may be used to advantage in the generation of the laterally moving jets of cryptosteady-flow thrust augmenters' and energy separators. To this end, the primary fluid wo
Autor:
Joseph V. Foa
Publikováno v:
AIAA Journal. 1:466-467
Autor:
Joseph V. Foa
Publikováno v:
Journal of Fluids Engineering. 80:1035-1036
Autor:
Joseph V. Foa
Publikováno v:
Journal of Basic Engineering. 82:570-571
Autor:
Joseph V. Foa
Publikováno v:
Journal of Propulsion and Power. 4:598-598