Author

M. J. Abbett

Observed names: M. ABBETT, M. Abbett, MICHAEL ABBETT, MICHAEL J. ABBETT, Michael J. Abbett

Institution: Applied Science Laboratories (United States)

Observed institution: Applied Science Laboratories (United States)

OpenAlex ID: A5111969969

Mach disk in underexpanded exhaust plumes

1971 · MICHAEL ABBETT · AIAA Journal · 79

Boundary condition computational procedures for inviscid, supersonic steady flow field calculations

1971 · M. J. Abbett · NASA Technical Reports Server (NASA) · 32

Boundary Condition Calculation Procedures for Inviscid Supersonic Flow Fields*

1973 · MICHAEL ABBETT · AIAA Computational Fluid Dynamics Conference · 28

A computation of one-dimensional combustion of methane

1965 · JAMES J. DEGROAT, MICHAEL J. ABBETT · AIAA Journal · 26

A Time-Dependent Computaional Method for Blunt Body Flows

2003 · GINO MORETTI, MICHAEL ABBETT · Journal of Spacecraft and Rockets · 23

Flow characteristics about concave conic forebodies at high Mach number

1975 · M. ABBETT, L. COOPER, et al. · AIAA Aerospace Sciences Meeting · 13

Viscous effects on blast wave flowfields

1986 · B. BENNETT, M. ABBETT, et al. · 24th Aerospace Sciences Meeting · 4

Three-Dimensional Inviscid Flow About Supersonic Blunt Cones at Angle of Attack, III: Coupled Subsonic and Supersonic Programs for Inviscid Three-Dimensional Flow

1968 · M. Abbett, R. Fort · OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information) · 4

Passive Nosetip Technology (PANT) Program. Volume 20. Investigation of Flow Phenomena over Reentry Vehicle Nosetips

1975 · M. J. Abbett, A. D. Anderson, et al. · Defense Technical Information Center (DTIC) · 3

The Mach disc in underexpanded exhaust plumes

1970 · M. ABBETT · 8th Aerospace Sciences Meeting · 3

Flow Characteristics about Concave Conic Forebodies at M^ = 5

1975 · Michael J. Abbett, Larry Cooper, et al. · AIAA Journal · 2

Three-Dimensional Compressible Boundary Layers of Reacting Gases Over Realistic Configurations

1975 · R. M. Kendall, W. S. Bonnett, et al. · 2

Computational procedure for three-dimensional boundary layers on aircraft and aerospace vehicles

1975 · R. M. Kendall, W. S. Bonnett, et al. · NASA Technical Reports Server (NASA) · 2

Finite Difference Solution of the Subsonic/Supersonic Inviscid Flow Field about a Supersonic, Axisymmetric Blunt Body at Zero Incidence - Analysis and User's Manual

1971 · SNL (Sandia National Laboratories (SNL), Albuquerque, NM, and Livermore, CA (United States)), M. Abbett, et al. · OSTI OAI (U.S. Department of Energy Office of Scientific and Technical Information) · 2

Some aspects of viscous chemically reacting moderate altitude rocket exhaust plumes Final report

1970 · M. J. Abbett, R. B. Edelman, et al. · NASA STI Repository (National Aeronautics and Space Administration) · 2

Non-equilibrium effects for quasi-equilibrium flows in nozzles

1966 · M. ABBETT · AIAA/SAE Propulsion Joint Specialist Conference · 1

Calculation of three-dimensional compressible laminar and turbulent boundary flows. Three-dimensional compressible boundary layers of reacting gases over realistic configurations

1975 · R. M. Kendall, W. S. Bonnett, et al. · NASA Technical Reports Server (NASA)

Works count: 17

Citation count: 226

H-index: 6

I10-index: 6