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Source: The Open Library

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1High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)

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“High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)” Metadata:

  • Title: ➤  High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)
  • Author:
  • Language: English
  • Number of Pages: Median: 537
  • Publisher: ➤  AIAA (American Institute of Aeronautics & Ast
  • Publish Date:
  • Dewey Decimal Classification:
  • Library of Congress Classification: TL-0507.00000000.P75 v. 137

“High-Speed Flight Propulsion Systems (Progress in Astronautics and Aeronautics)” Subjects and Themes:

Edition Identifiers:

Book Classifications

Access and General Info:

  • First Year Published: 1991
  • Is Full Text Available: Yes
  • Is The Book Public: No
  • Access Status: Borrowable

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2Practical intake aerodynamic design

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“Practical intake aerodynamic design” Metadata:

  • Title: ➤  Practical intake aerodynamic design
  • Authors:
  • Language: English
  • Number of Pages: Median: 434
  • Publisher: ➤  Blackwell Scientific Publications - American Institute of Aeronautics and Astronautics
  • Publish Date:
  • Publish Location: Oxford, UK - Washington, DC
  • Dewey Decimal Classification: 629.134353
  • Library of Congress Classification: TL-0709.50000000.I15 P72 1993

“Practical intake aerodynamic design” Subjects and Themes:

Edition Identifiers:

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Access and General Info:

  • First Year Published: 1993
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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3Turbofan forced mixer-nozzle internal flowfield

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“Turbofan forced mixer-nozzle internal flowfield” Metadata:

  • Title: ➤  Turbofan forced mixer-nozzle internal flowfield
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Washington, D.C

“Turbofan forced mixer-nozzle internal flowfield” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1982
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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4Practical intake aerodynamic design

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Book's cover

“Practical intake aerodynamic design” Metadata:

  • Title: ➤  Practical intake aerodynamic design
  • Authors:
  • Language: English
  • Number of Pages: Median: 434
  • Publisher: ➤  American Institute of Aeronautics and Astronautics - Amer Inst of Aeronautics & - Blackwell Scientific Publications
  • Publish Date:
  • Publish Location: Washington, DC - Oxford, UK
  • Dewey Decimal Classification: 629.134353
  • Library of Congress Classification: TL-0709.50000000.I15 P72 1993TL-0709.50000000.I15P72 1993

“Practical intake aerodynamic design” Subjects and Themes:

Edition Identifiers:

Book Classifications

Access and General Info:

  • First Year Published: 1993
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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5CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system

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“CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Metadata:

  • Title: ➤  CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
  • Author:
  • Language: English
  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  Springfield, Va - [Washington, DC

“CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Subjects and Themes:

Edition Identifiers:

Access and General Info:

  • First Year Published: 1997
  • Is Full Text Available: No
  • Is The Book Public: No
  • Access Status: No_ebook

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    6Analysis of a new rocket-based combined-cycle engine concept at low speed

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    “Analysis of a new rocket-based combined-cycle engine concept at low speed” Metadata:

    • Title: ➤  Analysis of a new rocket-based combined-cycle engine concept at low speed
    • Author:
    • Language: English
    • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

    “Analysis of a new rocket-based combined-cycle engine concept at low speed” Subjects and Themes:

    Edition Identifiers:

    Access and General Info:

    • First Year Published: 1999
    • Is Full Text Available: No
    • Is The Book Public: No
    • Access Status: No_ebook

    Online Access

    Downloads Are Not Available:

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      7Control of aircraft and missile powerplants

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      “Control of aircraft and missile powerplants” Metadata:

      • Title: ➤  Control of aircraft and missile powerplants
      • Author:
      • Language: English
      • Number of Pages: Median: 432
      • Publisher: Wiley
      • Publish Date:
      • Publish Location: New York
      • Dewey Decimal Classification: 629.13435
      • Library of Congress Classification: TL-0709.50000000.C57 S6

      “Control of aircraft and missile powerplants” Subjects and Themes:

      Edition Identifiers:

      Book Classifications

      Access and General Info:

      • First Year Published: 1963
      • Is Full Text Available: Yes
      • Is The Book Public: No
      • Access Status: Printdisabled

      Online Access

      Downloads Are Not Available:

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        8Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

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        “Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” Metadata:

        • Title: ➤  Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft
        • Author:
        • Language: English
        • Number of Pages: Median: 10
        • Publisher: ➤  For sale by the National Technical Information Service - NASA
        • Publish Date:
        • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

        “Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 1990
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

        Downloads Are Not Available:

        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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          9Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

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          “Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” Metadata:

          • Title: ➤  Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
          • Author:
          • Language: English
          • Number of Pages: Median: 101
          • Publisher: ➤  for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
          • Publish Date:
          • Publish Location: [Washington] - Springfield, Va

          “Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1978
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          10Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6

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          “Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Metadata:

          • Title: ➤  Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6
          • Author:
          • Language: English
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
          • Publish Date:
          • Publish Location: ➤  [Springfield, Va - Washington, D.C

          “Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1979
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Marketplaces

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          11Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles

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          “Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles” Metadata:

          • Title: ➤  Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles
          • Author:
          • Language: English
          • Number of Pages: Median: 181
          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office
          • Publish Date:
          • Publish Location: ➤  Springfield, Va. : for sale by the National Technical Information Service - [Washington]

          “Flight effects on the aerodynamic and acoustic characteristics of inverted profile coannular nozzles” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1978
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          12Hypersonic airbreathing propulsion

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          Book's cover

          “Hypersonic airbreathing propulsion” Metadata:

          • Title: ➤  Hypersonic airbreathing propulsion
          • Author:
          • Language: English
          • Number of Pages: Median: 587
          • Publisher: ➤  American Institute of Aeronautics and Astronautics
          • Publish Date:
          • Publish Location: Washington, D.C
          • Dewey Decimal Classification: 629.1343535
          • Library of Congress Classification: TL-0709.00000000.H38 1994TL-0709.00000000TL-0709.00000000.H38 1994eb

          “Hypersonic airbreathing propulsion” Subjects and Themes:

          Edition Identifiers:

          Book Classifications

          Access and General Info:

          • First Year Published: 1994
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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          13Developments in high-speed-vehicle propusion systems

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          Book's cover

          “Developments in high-speed-vehicle propusion systems” Metadata:

          • Title: ➤  Developments in high-speed-vehicle propusion systems
          • Author:
          • Language: English
          • Number of Pages: Median: 699
          • Publisher: ➤  American Institute of Aeronautics and Astronautics, Inc. - AIAA (American Institute of Aeronautics & Ast
          • Publish Date:
          • Publish Location: Reston, Virginia

          “Developments in high-speed-vehicle propusion systems” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1996
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

          Online Access

          Downloads Are Not Available:

          The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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            14Aerospace propulsion systems

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            Book's cover

            “Aerospace propulsion systems” Metadata:

            • Title: Aerospace propulsion systems
            • Author:
            • Language: English
            • Publisher: Wiley
            • Publish Date:
            • Publish Location: Singapore - Hoboken, NJ
            • Dewey Decimal Classification: 629.13435
            • Library of Congress Classification: TL-0701.00000000.W345 2010TL-0782.00000000

            “Aerospace propulsion systems” Subjects and Themes:

            Edition Identifiers:

            Book Classifications

            Access and General Info:

            • First Year Published: 2010
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            15Virtualʹnye aviadvigateli

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            “Virtualʹnye aviadvigateli” Metadata:

            • Title: Virtualʹnye aviadvigateli
            • Author:
            • Language: rus
            • Number of Pages: Median: 34
            • Publisher: ➤  Vychislitelʹnyĭ T︠S︡entr im. A.A. Dorodnit︠s︡yna Rossiĭskoĭ akademii nauk - Vychislitelʹnyĭ t︠s︡entr im. A.A. Dorodnit︠s︡ina Rossiĭskoĭ akademii nauk
            • Publish Date:
            • Publish Location: Moskva
            • Dewey Decimal Classification:
            • Library of Congress Classification: TL-0709.00000000.Z54 2012TL-0709.30000000.T83 Z59 2010

            “Virtualʹnye aviadvigateli” Subjects and Themes:

            Edition Identifiers:

            Book Classifications

            Access and General Info:

            • First Year Published: 2010
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

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            16Analysis of internal flow in a ventral nozzle for STOVL aircraft

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            “Analysis of internal flow in a ventral nozzle for STOVL aircraft” Metadata:

            • Title: ➤  Analysis of internal flow in a ventral nozzle for STOVL aircraft
            • Author:
            • Language: English
            • Number of Pages: Median: 19
            • Publisher: ➤  For sale by the National Technical Information Service - NASA
            • Publish Date:
            • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

            “Analysis of internal flow in a ventral nozzle for STOVL aircraft” Subjects and Themes:

            Edition Identifiers:

            Access and General Info:

            • First Year Published: 1990
            • Is Full Text Available: No
            • Is The Book Public: No
            • Access Status: No_ebook

            Online Access

            Downloads Are Not Available:

            The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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              17Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6

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              “Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Metadata:

              • Title: ➤  Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
              • Publish Date:
              • Publish Location: ➤  [Springfield, Va - Washington, D.C

              “Flight-measured afterbody pressure coefficients from an airplane having twin side-by-side jet engines for Mach numbers from 0.6 to 1.6” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1979
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Marketplaces

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              18Modifications to the nozzle test chamber to extend nozzle static-test capability

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              “Modifications to the nozzle test chamber to extend nozzle static-test capability” Metadata:

              • Title: ➤  Modifications to the nozzle test chamber to extend nozzle static-test capability
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
              • Publish Date:
              • Publish Location: [Washington, D.C.?]

              “Modifications to the nozzle test chamber to extend nozzle static-test capability” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

              • First Year Published: 1985
              • Is Full Text Available: No
              • Is The Book Public: No
              • Access Status: No_ebook

              Online Access

              Downloads Are Not Available:

              The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                19René Leduc, pionnier de la propulsion à réaction

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                Book's cover

                “René Leduc, pionnier de la propulsion à réaction” Metadata:

                • Title: ➤  René Leduc, pionnier de la propulsion à réaction
                • Authors:
                • Language: fre
                • Number of Pages: Median: 256
                • Publisher: Larivière - La Rivière
                • Publish Date:
                • Publish Location: Clichy
                • Dewey Decimal Classification: 629.130092
                • Library of Congress Classification: TL-0540.00000000.L375 L33 2000

                “René Leduc, pionnier de la propulsion à réaction” Subjects and Themes:

                Edition Identifiers:

                Book Classifications

                Access and General Info:

                • First Year Published: 2000
                • Is Full Text Available: No
                • Is The Book Public: No
                • Access Status: No_ebook

                Online Access

                Downloads Are Not Available:

                The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                  20Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft

                  By

                  “Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft” Metadata:

                  • Title: ➤  Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft
                  • Author:
                  • Language: English
                  • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                  • Publish Date:
                  • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                  “Experimental performance of a ventral nozzle with pitch and yaw vectoring capability for SSTOVL aircraft” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 1993
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Access

                  Downloads Are Not Available:

                  The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                    21Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft

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                    “Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft” Metadata:

                    • Title: ➤  Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft
                    • Author:
                    • Language: English
                    • Number of Pages: Median: 14
                    • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                    • Publish Date:
                    • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                    “Experimental performance of three design factors for ventral nozzles for SSTOVL aircraft” Subjects and Themes:

                    Edition Identifiers:

                    Access and General Info:

                    • First Year Published: 1992
                    • Is Full Text Available: No
                    • Is The Book Public: No
                    • Access Status: No_ebook

                    Online Access

                    Downloads Are Not Available:

                    The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                      22Comparison of combustion efficiencies for ramjet engines

                      By

                      “Comparison of combustion efficiencies for ramjet engines” Metadata:

                      • Title: ➤  Comparison of combustion efficiencies for ramjet engines
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration
                      • Publish Date:
                      • Publish Location: Washington, D.C

                      “Comparison of combustion efficiencies for ramjet engines” Subjects and Themes:

                      Edition Identifiers:

                      Access and General Info:

                      • First Year Published: 1984
                      • Is Full Text Available: No
                      • Is The Book Public: No
                      • Access Status: No_ebook

                      Online Access

                      Downloads Are Not Available:

                      The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                        23Inlets for supersonic missiles

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                        Book's cover

                        “Inlets for supersonic missiles” Metadata:

                        • Title: Inlets for supersonic missiles
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 237
                        • Publisher: ➤  Amer Inst of Aeronautics & - American Institute of Aeronautics and Astronautics
                        • Publish Date:
                        • Publish Location: Washington, D.C
                        • Dewey Decimal Classification: 623.4519
                        • Library of Congress Classification: TL-0709.30000000.R3 M34 1990TL-0709.30000000.R3M34 1990

                        “Inlets for supersonic missiles” Subjects and Themes:

                        Edition Identifiers:

                        Book Classifications

                        Access and General Info:

                        • First Year Published: 1990
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

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                        24Mach 10 experimental database of a three-dimensional scramjet inlet flow field

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                        “Mach 10 experimental database of a three-dimensional scramjet inlet flow field” Metadata:

                        • Title: ➤  Mach 10 experimental database of a three-dimensional scramjet inlet flow field
                        • Author:
                        • Language: English
                        • Number of Pages: Median: 214
                        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - Available from the National Technical Information Service
                        • Publish Date:
                        • Publish Location: ➤  [Springfield, VA - Springfield, VA - Hampton, Va

                        “Mach 10 experimental database of a three-dimensional scramjet inlet flow field” Subjects and Themes:

                        Edition Identifiers:

                        Access and General Info:

                        • First Year Published: 1995
                        • Is Full Text Available: No
                        • Is The Book Public: No
                        • Access Status: No_ebook

                        Online Access

                        Downloads Are Not Available:

                        The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.

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                          25Some fundamentals on the performance of ramjets with subsonic and supersonic combustion

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                          “Some fundamentals on the performance of ramjets with subsonic and supersonic combustion” Metadata:

                          • Title: ➤  Some fundamentals on the performance of ramjets with subsonic and supersonic combustion
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 189
                          • Publisher: TNO Prins Maurits Laboratory
                          • Publish Date:
                          • Publish Location: Rijswijk, The Netherlands

                          “Some fundamentals on the performance of ramjets with subsonic and supersonic combustion” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 2000
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                          26Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control

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                          “Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” Metadata:

                          • Title: ➤  Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control
                          • Author:
                          • Language: English
                          • Number of Pages: Median: 101
                          • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
                          • Publish Date:
                          • Publish Location: Springfield, Va - [Washington]

                          “Wind-tunnel investigations at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control” Subjects and Themes:

                          Edition Identifiers:

                          Access and General Info:

                          • First Year Published: 1978
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

                          Online Marketplaces

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                          27Hypersonic airbreathing propulsion

                          Book's cover

                          “Hypersonic airbreathing propulsion” Metadata:

                          • Title: ➤  Hypersonic airbreathing propulsion
                          • Language: English
                          • Number of Pages: Median: 587
                          • Publisher: ➤  AIAA (American Institute of Aeronautics & Ast
                          • Publish Date:

                          “Hypersonic airbreathing propulsion” Subjects and Themes:

                          Edition Identifiers:

                          First Setence:

                          "The subject of this book is the hypersonic airbreathing engine, a device that employs the enveloping atmosphere to propel aerospace vehicles at sustained speeds greatly in excess of the local speed of sound."

                          Access and General Info:

                          • First Year Published: 1993
                          • Is Full Text Available: No
                          • Is The Book Public: No
                          • Access Status: No_ebook

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                            28Preliminary calibration of a generic scramjet combustor

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                            “Preliminary calibration of a generic scramjet combustor” Metadata:

                            • Title: ➤  Preliminary calibration of a generic scramjet combustor
                            • Author:
                            • Number of Pages: Median: 28
                            • Publisher: ➤  Institute for Computer Applications in Science and Engineering
                            • Publish Date:
                            • Publish Location: Hampton, Va

                            “Preliminary calibration of a generic scramjet combustor” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1991
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                            29Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi

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                            “Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi” Metadata:

                            • Title: ➤  Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi
                            • Author: ➤  
                            • Language: rus
                            • Number of Pages: Median: 260
                            • Publisher: Mashinostroenie
                            • Publish Date:
                            • Publish Location: Moskva
                            • Dewey Decimal Classification:
                            • Library of Congress Classification: TL-0709.30000000.R3 P6

                            “Silovye ustanovki letatel'nykh apparatov s vozdushno-reaktivnymi dvigateli͡a︡mi” Subjects and Themes:

                            Edition Identifiers:

                            • The Open Library ID: OL5554710M
                            • Online Computer Library Center (OCLC) ID: 30350103
                            • Library of Congress Control Number (LCCN): 67040226

                            Book Classifications

                            Access and General Info:

                            • First Year Published: 1965
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                            30Viscous flow simulations of internal store carriage and separation

                            By

                            “Viscous flow simulations of internal store carriage and separation” Metadata:

                            • Title: ➤  Viscous flow simulations of internal store carriage and separation
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Aeronautics and Space Administration - Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University
                            • Publish Date:
                            • Publish Location: Norfolk, Va - [Washington, D.C

                            “Viscous flow simulations of internal store carriage and separation” Subjects and Themes:

                            Edition Identifiers:

                            Access and General Info:

                            • First Year Published: 1991
                            • Is Full Text Available: No
                            • Is The Book Public: No
                            • Access Status: No_ebook

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                              31The design and performance estimates for the propulsion module for the booster of a TSTO vehicle

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                              “The design and performance estimates for the propulsion module for the booster of a TSTO vehicle” Metadata:

                              • Title: ➤  The design and performance estimates for the propulsion module for the booster of a TSTO vehicle
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Technical Information Service [distributor] - National Aeronautics and Space Administration
                              • Publish Date:
                              • Publish Location: ➤  [Washington, DC] - [Springfield, Va.?

                              “The design and performance estimates for the propulsion module for the booster of a TSTO vehicle” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1991
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

                              Online Access

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                                32A parametric study of a gas-generator airturbo ramjet (ATR)

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                                “A parametric study of a gas-generator airturbo ramjet (ATR)” Metadata:

                                • Title: ➤  A parametric study of a gas-generator airturbo ramjet (ATR)
                                • Author:
                                • Language: English
                                • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration
                                • Publish Date:
                                • Publish Location: ➤  [Washington, DC] - [Springfield, Va

                                “A parametric study of a gas-generator airturbo ramjet (ATR)” Subjects and Themes:

                                Edition Identifiers:

                                Access and General Info:

                                • First Year Published: 1986
                                • Is Full Text Available: No
                                • Is The Book Public: No
                                • Access Status: No_ebook

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                                  33Contribution à l'etude aérodynamique du statoréacteur subsonique

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                                  “Contribution à l'etude aérodynamique du statoréacteur subsonique” Metadata:

                                  • Title: ➤  Contribution à l'etude aérodynamique du statoréacteur subsonique
                                  • Author:
                                  • Language: fre
                                  • Number of Pages: Median: 49
                                  • Publisher: ➤  En vente au Service de documentation et d'information technique de l'aéronautique
                                  • Publish Date:
                                  • Publish Location: Paris
                                  • Dewey Decimal Classification:
                                  • Library of Congress Classification: TL-0502.00000000.F77 no. 253

                                  “Contribution à l'etude aérodynamique du statoréacteur subsonique” Subjects and Themes:

                                  Edition Identifiers:

                                  • The Open Library ID: OL6151686M
                                  • Online Computer Library Center (OCLC) ID: 6733326
                                  • Library of Congress Control Number (LCCN): 54004040

                                  Book Classifications

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                                  • First Year Published: 1951
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  34Le statoréacteur supersonique aux nombres de Mach modérés

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                                  “Le statoréacteur supersonique aux nombres de Mach modérés” Metadata:

                                  • Title: ➤  Le statoréacteur supersonique aux nombres de Mach modérés
                                  • Author:
                                  • Language: fre
                                  • Number of Pages: Median: 103
                                  • Publisher: ➤  En vente au Service de documentation et d'information technique de l'aéronautique
                                  • Publish Date:
                                  • Publish Location: Paris
                                  • Dewey Decimal Classification:
                                  • Library of Congress Classification: TL-0502.00000000.F77 no. 274

                                  “Le statoréacteur supersonique aux nombres de Mach modérés” Subjects and Themes:

                                  Edition Identifiers:

                                  • The Open Library ID: OL6151687M
                                  • Online Computer Library Center (OCLC) ID: 7631736
                                  • Library of Congress Control Number (LCCN): 54004041

                                  Book Classifications

                                  Access and General Info:

                                  • First Year Published: 1952
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  35Ispytanii͡a︡ vozdushno-reaktivnykh dvigateleĭ

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                                  “Ispytanii͡a︡ vozdushno-reaktivnykh dvigateleĭ” Metadata:

                                  • Title: ➤  Ispytanii͡a︡ vozdushno-reaktivnykh dvigateleĭ
                                  • Author: ➤  
                                  • Language: rus
                                  • Number of Pages: Median: 220
                                  • Publisher: Oborongiz
                                  • Publish Date:
                                  • Publish Location: Moskva
                                  • Dewey Decimal Classification:
                                  • Library of Congress Classification: TL-0709.30000000.R3 D6

                                  “Ispytanii͡a︡ vozdushno-reaktivnykh dvigateleĭ” Subjects and Themes:

                                  Edition Identifiers:

                                  • The Open Library ID: OL5863086M
                                  • Online Computer Library Center (OCLC) ID: 4015005
                                  • Library of Congress Control Number (LCCN): 62038192

                                  Book Classifications

                                  Access and General Info:

                                  • First Year Published: 1961
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  36Teorii͡a︡ pri͡a︡motochnykh i raketno-pri͡a︡motochnykh dvigatelĭ

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                                  “Teorii͡a︡ pri͡a︡motochnykh i raketno-pri͡a︡motochnykh dvigatelĭ” Metadata:

                                  • Title: ➤  Teorii͡a︡ pri͡a︡motochnykh i raketno-pri͡a︡motochnykh dvigatelĭ
                                  • Author:
                                  • Language: rus
                                  • Number of Pages: Median: 367
                                  • Publisher: "Mashinostroenie,"
                                  • Publish Date:
                                  • Publish Location: Moskva
                                  • Dewey Decimal Classification:
                                  • Library of Congress Classification: TL-0709.30000000.R3 Z84

                                  “Teorii͡a︡ pri͡a︡motochnykh i raketno-pri͡a︡motochnykh dvigatelĭ” Subjects and Themes:

                                  Edition Identifiers:

                                  • The Open Library ID: OL5359245M
                                  • Online Computer Library Center (OCLC) ID: 30372269
                                  • Library of Congress Control Number (LCCN): 72320488

                                  Book Classifications

                                  Access and General Info:

                                  • First Year Published: 1971
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  37Application of the ram jet to vertical ascent

                                  By

                                  “Application of the ram jet to vertical ascent” Metadata:

                                  • Title: ➤  Application of the ram jet to vertical ascent
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 53
                                  • Publish Date:
                                  • Publish Location: Pasadena
                                  • Dewey Decimal Classification: 629.13338
                                  • Library of Congress Classification: TL-0782.00000000.R69

                                  “Application of the ram jet to vertical ascent” Subjects and Themes:

                                  Edition Identifiers:

                                  • The Open Library ID: OL6101631M
                                  • Online Computer Library Center (OCLC) ID: 6226959
                                  • Library of Congress Control Number (LCCN): 51033693

                                  Book Classifications

                                  Access and General Info:

                                  • First Year Published: 1950
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  38Theoretical and experimental analysis of low-drag supersonic inlets having a circular cross section and a central body at Mach numbers of 3.30, 2.75, and 2.45

                                  By

                                  “Theoretical and experimental analysis of low-drag supersonic inlets having a circular cross section and a central body at Mach numbers of 3.30, 2.75, and 2.45” Metadata:

                                  • Title: ➤  Theoretical and experimental analysis of low-drag supersonic inlets having a circular cross section and a central body at Mach numbers of 3.30, 2.75, and 2.45
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 37
                                  • Publisher: U.S. Govt. Print. Off.
                                  • Publish Date:
                                  • Publish Location: Washington
                                  • Dewey Decimal Classification: 629.13008 s629.134353
                                  • Library of Congress Classification: TL-0521.00000000.A33 no. 1189

                                  “Theoretical and experimental analysis of low-drag supersonic inlets having a circular cross section and a central body at Mach numbers of 3.30, 2.75, and 2.45” Subjects and Themes:

                                  Edition Identifiers:

                                  Book Classifications

                                  Access and General Info:

                                  • First Year Published: 1955
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  39Supersonic inlet diffusers and introduction to internal aerodynamics

                                  By

                                  “Supersonic inlet diffusers and introduction to internal aerodynamics” Metadata:

                                  • Title: ➤  Supersonic inlet diffusers and introduction to internal aerodynamics
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 378
                                  • Publisher: ➤  Minneapolis-Honeywell Regulator Co., Aeronautical Division
                                  • Publish Date:
                                  • Publish Location: Minneapolis
                                  • Dewey Decimal Classification: 629.1323629.123*
                                  • Library of Congress Classification: TL-0709.50000000.D5 H4

                                  “Supersonic inlet diffusers and introduction to internal aerodynamics” Subjects and Themes:

                                  Edition Identifiers:

                                  • The Open Library ID: OL6217573M
                                  • Online Computer Library Center (OCLC) ID: 2999638
                                  • Library of Congress Control Number (LCCN): 57000694

                                  Book Classifications

                                  Access and General Info:

                                  • First Year Published: 1956
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  40Un homme seul, René Leduc

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                                  “Un homme seul, René Leduc” Metadata:

                                  • Title: Un homme seul, René Leduc
                                  • Author:
                                  • Language: fre
                                  • Number of Pages: Median: 283
                                  • Publisher: Officine
                                  • Publish Date:
                                  • Publish Location: Paris

                                  “Un homme seul, René Leduc” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 2004
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  41Evaluation of bulk calorimeter and heat balance for determination of supersonic combustor efficiency

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                                  “Evaluation of bulk calorimeter and heat balance for determination of supersonic combustor efficiency” Metadata:

                                  • Title: ➤  Evaluation of bulk calorimeter and heat balance for determination of supersonic combustor efficiency
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 42
                                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                                  • Publish Date:
                                  • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                  “Evaluation of bulk calorimeter and heat balance for determination of supersonic combustor efficiency” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1980
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  42Expanded operational capabilities of the Langley Mach 7 scramjet test facility

                                  By

                                  “Expanded operational capabilities of the Langley Mach 7 scramjet test facility” Metadata:

                                  • Title: ➤  Expanded operational capabilities of the Langley Mach 7 scramjet test facility
                                  • Author:
                                  • Language: English
                                  • Number of Pages: Median: 71
                                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
                                  • Publish Date:
                                  • Publish Location: ➤  [Springfield, Va - Washington, D.C

                                  “Expanded operational capabilities of the Langley Mach 7 scramjet test facility” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1983
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                  43Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds

                                  By

                                  “Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds” Metadata:

                                  • Title: ➤  Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                  • Publish Date:
                                  • Publish Location: [Washington, D.C.?]

                                  “Fuselage and nozzle pressure distributions of a 1/12-scale f-15 propulsion model at transonic speeds” Subjects and Themes:

                                  Edition Identifiers:

                                  Access and General Info:

                                  • First Year Published: 1984
                                  • Is Full Text Available: No
                                  • Is The Book Public: No
                                  • Access Status: No_ebook

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                                    44Computational analysis of scramjet dual mode operation

                                    By

                                    “Computational analysis of scramjet dual mode operation” Metadata:

                                    • Title: ➤  Computational analysis of scramjet dual mode operation
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  Dept. of Aeronautics and Astronautics, Massachusetts Institute of Technology
                                    • Publish Date:
                                    • Publish Location: Cambridge, Mass

                                    “Computational analysis of scramjet dual mode operation” Subjects and Themes:

                                    Edition Identifiers:

                                    Access and General Info:

                                    • First Year Published: 1985
                                    • Is Full Text Available: No
                                    • Is The Book Public: No
                                    • Access Status: No_ebook

                                    Online Access

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                                      45Ignition of mixtures of SiH4, CH4, O2, and Ar or N2 behind reflected shock waves

                                      By

                                      “Ignition of mixtures of SiH4, CH4, O2, and Ar or N2 behind reflected shock waves” Metadata:

                                      • Title: ➤  Ignition of mixtures of SiH4, CH4, O2, and Ar or N2 behind reflected shock waves
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service,]
                                      • Publish Date:
                                      • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                                      “Ignition of mixtures of SiH4, CH4, O2, and Ar or N2 behind reflected shock waves” Subjects and Themes:

                                      Edition Identifiers:

                                      Access and General Info:

                                      • First Year Published: 1985
                                      • Is Full Text Available: No
                                      • Is The Book Public: No
                                      • Access Status: No_ebook

                                      Online Access

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                                        46Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system

                                        By

                                        “Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system” Metadata:

                                        • Title: ➤  Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
                                        • Publish Date:
                                        • Publish Location: ➤  Springfield, VA - [Cleveland, Ohio]

                                        “Parametric studies of the ejector process within a turbine-based combined-cycle propulsion system” Subjects and Themes:

                                        Edition Identifiers:

                                        Access and General Info:

                                        • First Year Published: 1999
                                        • Is Full Text Available: No
                                        • Is The Book Public: No
                                        • Access Status: No_ebook

                                        Online Access

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                                          47Progress toward synergistic hypermixing nozzles

                                          By

                                          “Progress toward synergistic hypermixing nozzles” Metadata:

                                          • Title: ➤  Progress toward synergistic hypermixing nozzles
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: [Washington, DC]

                                          “Progress toward synergistic hypermixing nozzles” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1991
                                          • Is Full Text Available: No
                                          • Is The Book Public: No
                                          • Access Status: No_ebook

                                          Online Access

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                                            48Numerical simulation of reacting flow in a thermally choked ram accelerator

                                            By

                                            “Numerical simulation of reacting flow in a thermally choked ram accelerator” Metadata:

                                            • Title: ➤  Numerical simulation of reacting flow in a thermally choked ram accelerator
                                            • Author:
                                            • Number of Pages: Median: 52
                                            • Publisher: Ballistic Research Laboratory
                                            • Publish Date:
                                            • Publish Location: Aberdeen Proving Ground, Md

                                            “Numerical simulation of reacting flow in a thermally choked ram accelerator” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

                                            • First Year Published: 1991
                                            • Is Full Text Available: No
                                            • Is The Book Public: No
                                            • Access Status: No_ebook

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                                            49Suppression of premature ignition in the pre-mixed inlet flow of a shcramjet

                                            By

                                            “Suppression of premature ignition in the pre-mixed inlet flow of a shcramjet” Metadata:

                                            • Title: ➤  Suppression of premature ignition in the pre-mixed inlet flow of a shcramjet
                                            • Author:
                                            • Language: English
                                            • Number of Pages: Median: 93
                                            • Publisher: ➤  University of Toronto, Institute for Aerospace Studies
                                            • Publish Date:
                                            • Publish Location: [Downsview, Ont.]

                                            “Suppression of premature ignition in the pre-mixed inlet flow of a shcramjet” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

                                            • First Year Published: 2003
                                            • Is Full Text Available: No
                                            • Is The Book Public: No
                                            • Access Status: No_ebook

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                                            50Combustion behavior of solid fuel ramjets, vol. 1. Correlation of reacting and non-reacting flow characteristics

                                            By

                                            Book's cover

                                            “Combustion behavior of solid fuel ramjets, vol. 1. Correlation of reacting and non-reacting flow characteristics” Metadata:

                                            • Title: ➤  Combustion behavior of solid fuel ramjets, vol. 1. Correlation of reacting and non-reacting flow characteristics
                                            • Author:
                                            • Language: English
                                            • Number of Pages: Median: 58
                                            • Publisher: Naval Postgraduate School
                                            • Publish Date:
                                            • Publish Location: Monterey, Calif

                                            “Combustion behavior of solid fuel ramjets, vol. 1. Correlation of reacting and non-reacting flow characteristics” Subjects and Themes:

                                            Edition Identifiers:

                                            Access and General Info:

                                            • First Year Published: 1981
                                            • Is Full Text Available: Yes
                                            • Is The Book Public: Yes
                                            • Access Status: Public

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