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  • Author > Ferri, A. [x]

  • Sort results by: NASA Center | Date Added to NTRS | Publication Year
    There are a total of 45 record(s) matching your query.
    Sorted by: Date Added To NTRS in Descending order

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    Review of problems in application of supersonic combustion.

    Author(s): Ferri, A.
    Abstract: Supersonic combustion ramjet design for hypersonic flight, examining combustion control, reaction and mixing processes
    NASA Center: NASA (non Center Specific)
    Publication Year: 1964
    Added to NTRS: 2006-11-06
    Accession Number: 64A25462; Document ID: 19640039569

    Mixing processes in supersonic combustion

    Author(s): Ferri, A.; Moretti, G.; Slutsky, S.
    Abstract: Fluid dynamics and chemistry of supersonic combustion in mixing process
    NASA Center: NASA (non Center Specific)
    Publication Year: 1964
    Added to NTRS: 2006-11-06
    Accession Number: 65N21457; Document ID: 19650011856; Report Number: NASA-CR-62194

    Review of problems in application of super- sonic combustion

    Author(s): Ferri, A.
    Abstract: Supersonic combustion ramjet engine - application to hypersonic flight
    NASA Center: NASA (non Center Specific)
    Publication Year: 1964
    Added to NTRS: 2006-11-06
    Accession Number: 65N12108; Document ID: 19650002507; Report Number: AD-604441, AFOSR-64-1471, NASA-CR-59662

    Mixing processes in supersonic combustion.

    Author(s): Ferri, A.; Moretti, G.; Slutsky, S.
    Abstract: Finite-rate chemistry of diffusion-controlled combustion in coupled supersonic hydrogen flows
    NASA Center: NASA (non Center Specific)
    Publication Year: 1965
    Added to NTRS: 2006-11-06
    Accession Number: 65A24670; Document ID: 19650041966

    Mixing processes in supersonic combustion

    Author(s): Ferri, A.; Moretti, G.; Slutsky, S.
    Abstract: Unmixed and premixed hydrogen chemical reactions in supersonic combustion for mathematical application of coupled axis flow problems
    NASA Center: NASA (non Center Specific)
    Publication Year: 1964
    Added to NTRS: 2006-11-06
    Accession Number: 65N18480; Document ID: 19650008879; Report Number: NASA-CR-57127

    Report on sonic boom studies - Part 1 - Analysis of configurations

    Author(s): Ferri, A.; Ismail, A.
    Abstract: Supersonic transport design and requirements for sonic boom reduction
    NASA Center: NASA (non Center Specific)
    Publication Year: 1968
    Added to NTRS: 2006-08-02
    Accession Number: 68N34915; Document ID: 19680025443

    Experimental verification of low sonic boom configuration

    Author(s): Ferri, A.; Wang, H. H.; Sorensen, H.
    Abstract: A configuration designed to produce near field signature has been tested at M = 2.71 and the results are analyzed, by taking in account three-dimensional and second order effects. The configuration has an equivalent total ...
    NASA Center: NASA (non Center Specific)
    Publication Year: 1972
    Added to NTRS: 2005-10-13
    Accession Number: 72N30007; Document ID: 19720022357; Report Number: NASA-CR-2070, NYU-AA-71-19

    Effect of premixing quality on oxides of nitrogen in gas turbine combustors foi HC

    Author(s): Roffe, G.; Ferri, A.
    Abstract: Experiments were conducted to determine the effectiveness of several premixing prevaporizing gas turbine combustor designs in reducing formation of oxides of nitrogen at the supersonic cruise condition. An atomized spray ...
    NASA Center: NASA (non Center Specific)
    Publication Year: 1976
    Added to NTRS: 2005-10-13
    Accession Number: 76N17149; Document ID: 19760010061; Report Number: NASA-CR-2657, TR-793

    Numerical program for analysis of three-dimensional supersonic exhaust flow fields (CHAR 3D)

    Author(s): Dash, S.; Guidice, P. D.; Ferri, A.; Roffe, G.
    Abstract: Choice of reference plane orientation depends on specific nozzle geometry, with different configurations requiring different reference plane systems. In addition, for given configuration several reference systems may be used ...
    NASA Center: Langley Research Center
    Publication Year: 1974
    Added to NTRS: 2005-09-30
    Accession Number: 74B10236; Document ID: 19740000236; Report Number: LAR-11596

    Integrated turbine-compressor provides air flow for cooling

    Author(s): Ferri, A.
    Abstract: Modified supersonic turbine cycle provides cooling air to surrounding structures. Simplified mechanical design assures correct balance of air flow, allows direct issue of cool air to the structure, and assists in matching ...
    NASA Center: NASA (non Center Specific)
    Publication Year: 1970
    Added to NTRS: 2005-09-30
    Accession Number: 70B10295; Document ID: 19700000284; Report Number: HQN-10442

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