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VITO D. AGOSTA
Observed names:
AGOSTA,Vito D.,
Agosta, V. D.,
Agosta, Vito D., author.,
Agosta,Vito D.,
V. AGOSTA,
V. D. Agosta,
Vito Agosta,
Vito D. Agosta
show all 8
Observed institution:
Jet Propulsion Laboratory
OpenAlex ID:
A5079232596
A Source Flow Model for Continuum Gas-Particle Flow
1967
·
David Migdal
, V. D. Agosta
·
Journal of Applied Mechanics
·
101
Effects of Emulsified Fuel on Combustion in a Four-Stroke Diesel Engine
1991
·
James A. Harbach
, Vito Agosta
·
Journal of Ship Research
·
54
Development of a fundamental model of hypergolic ignition in space-ambient engines.
1967
·
VITO D. AGOSTA
, THOMAS F. SEAMANS
, et al.
·
AIAA Journal
·
52
Spray Combustion Model With Droplet Breakup: Analytical and Experimental Results
1962
·
Samuel Z. Burstein
, Sanford S. Hammer
, et al.
·
Elsevier eBooks
·
9
Longitudinal wave propagation in liquid propellant rocket motors
1964
·
SANFORD S. HAMMER
, VITO D. AGOSTA
·
AIAA Journal
·
4
Combustion instability: Non-linear analysis of wave propagation in a liquid propellant rocket motor
1962
·
S. Z. Burstein
, V. D. Agosta
·
4
A fundamental model of hypergolic ignition in space-ambient engines
1966
·
V. AGOSTA
, T. SEAMANS
, et al.
·
3rd Annual Meeting
·
3
Wave slope-gas dynamic interactions in liquid rockets.
1966
·
VITO D. AGOSTA
, SANFORD S. HAMMER
·
AIAA Journal
·
3
Supersonic Gas-Particle Flow with Chemical Reactions
1967
·
David Migdal
, Vito D. Agosta
·
The Physics of Fluids
·
2
Vaporization response of evaporating drops with finite thermal conductivity
1975
·
V. D. Agosta
, S. Hammer
·
University of Michigan Library Repository
·
1
Droplet vaporization with liquid heat conduction Final report
1970
·
V. D. Agosta
, S. Hammer
·
NASA STI Repository (National Aeronautics and Space Administration)
PDF
Development of electroforming techniques for the fabrication of rocket engine injectors Final report, phase 2
1969
·
V. D. Agosta
, S. Hammer
·
NASA Technical Reports Server (NASA)
Supersonic gas-dynamic reacting flow systems
1968
·
V. AGOSTA
, S. HAMMER
·
AIAA Annual Meeting and Technical Display
Shock wave interaction with a burning solid propellant.
1966
·
VITO D. AGOSTA
·
AIAA Journal
Diffusion in a supersonic compressor stator by means of aerodynamic control
1965
·
VITO D. AGOSTA
·
Journal of Aircraft
Aerothermochemical analysis of non-oscillatory and oscillatory characteristics of liquid bipropellant rocket motors - droplet evaporation, wave equations, motor instrumentation, non-oscillatory program computation
1965
·
V. D. Agosta
, S. Z. Burstein
·
NASA Technical Reports Server (NASA)
PDF
Aerothermochemical analysis of non-oscillatory and oscillatory characteristics of liquid bipropellant rocket motors - Wave model, droplet heating, and evaporation program computation Third quarterly report no. 65-1
1965
·
V. D. Agosta
, S. Z. Burstein
·
NASA Technical Reports Server (NASA)
PDF
Steady state aerothermochemistry for liquid bipropellant rocket motors
1964
·
V. D. Agosta
, S. Z. Burstein
·
NASA Technical Reports Server (NASA)
PDF
Diffusion in a supersonic compressor stator by means of aerodynamic control
1964
·
V. AGOSTA
·
1st Annual Meeting
Shock-wave Propagation in Liquid Propellant Rocket Engines.
1961
·
AGOSTA,Vito D.
, Chinitz,Wallace
·
Defense Technical Information Center (DTIC)
Starting Characteristics of a Convergent-divergent Diffuser Blade Passage of a Supersonic Compressor in Mach Three Flow,
1960
·
Agosta,Vito D.
, DeCarlo,Joseph P.
·
Defense Technical Information Center (DTIC)
A theoretical investigation on the use of combustion products for the simulation of hypersonic flow /
1959
·
Agosta, Vito D., author.
, United States. Air Force. Air Research and Development Command, sponsor.
, et al.
·
University of Michigan Library Repository
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Works count:
23
Citation count:
233
H-index:
4
I10-index:
3
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