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Combustion Instability : Liquid Stream And Droplet Behavior. Part I: Experimental And Theoretical Analysis Of Evaporating Droplets
Author(s): Schuyler, Fred L.
Corporate Author(s): Aeronautical Research Laboratories
Laboratory: Aeronautical Research Laboratories
Date of Publication: 1960-09
Report number: WADC TR 59-720 Part 1
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Combustion Instability: Liquid Stream And Droplet Behavior. Part II. Estimationg Primary Liquid Breakup with Heat Transfer Considerations
Author(s): Imber, M.
Corporate Author(s): Aeronautical Research Laboratories
Laboratory: Aeronautical Research Laboratories
Date of Publication: 1960-09
Report number: WADC TR 59-720 Part 2
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Combustion Instability: Liquid Stream And Droplet Behavior. Part III: The Response Of Liquid Jets To Large Amplitude Sonic Oscillations
Author(s): Reba, Imants, Brosilow, Coleman
Corporate Author(s): Aeronautical Research Laboratories
Laboratory: Aeronautical Research Laboratories
Date of Publication: 1960-09
Report number: WADC TR 59-720 Part 3
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Basic Research On Gas Flows Through Electric Arcs-Hot Gas Containment Limits
Author(s): Cann, G. L., Buhler, R. D., Harder, R. L., Moore, R. A.
Corporate Author(s): Xerox Electro-Optical Systems Pasadena Ca
Laboratory: Aeronautical Research Laboratories
Date of Publication: 1964-03
Report number: ARL 64-49
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State-Of-The-Art Survey Of Some Aspects Of The Mechanics Of Rarefied Gases And Plasmas
Author(s): Patterson, G. N.
Corporate Author(s): Toronto Univ (Ontario)
Laboratory: Aeronautical Research Laboratories
Date of Publication: 1964-03
Report number: ARL 64-60
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Thermal Stresses Due To Large Spanwise Temperature Gradients In Long Thin Plates
Author(s): Gatewood, B. E., Dale, R. G., Glaser, A. R.
Corporate Author(s): Ohio State Univ Columbus
Laboratory: Aeronautical Research Laboratories
Date of Publication: 1963-01
Report number: ARL 63-4
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Numerical Analysis Of Supersonic Flow Through Curved Channels
Author(s): Der, J., Jr., Mullings, B. N., Hoffman, G. H., Brown, B. N. Pridmore
Corporate Author(s): Northrop Aircraft Inc Hawthorne Calif
Laboratory: Aeronautical Research Laboratories
Date of Publication: 1963-07
Report number: ARL 63-117

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