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1In-flight transport performance optimization

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“In-flight transport performance optimization” Metadata:

  • Title: ➤  In-flight transport performance optimization
  • Author:
  • Language: English
  • Number of Pages: Median: 15
  • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
  • Publish Date:
  • Publish Location: ➤  [Springfield, Va - Edwards, Calif

“In-flight transport performance optimization” 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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    2A reassessment of heavy-duty truck aerodynamic design features and priorities

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    “A reassessment of heavy-duty truck aerodynamic design features and priorities” Metadata:

    • Title: ➤  A reassessment of heavy-duty truck aerodynamic design features and priorities
    • Author:
    • Language: English
    • Number of Pages: Median: 32
    • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - Available from NASA Center for AeroSpace Information - National Technical Information Service, distributor
    • Publish Date:
    • Publish Location: ➤  [Springfield, Va - Edwards, Calif - Hanover, Md
    • Dewey Decimal Classification:
    • Library of Congress Classification: TL-0245.00000000 S33 1999

    “A reassessment of heavy-duty truck aerodynamic design features and priorities” Subjects and Themes:

    Edition Identifiers:

    Book Classifications

    Access and General Info:

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

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      3IPAC--Inlet Performance Analysis Code

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      “IPAC--Inlet Performance Analysis Code” Metadata:

      • Title: ➤  IPAC--Inlet Performance Analysis Code
      • Author:
      • Language: English
      • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
      • Publish Date:
      • Publish Location: ➤  Springfield, Va - [Washington, DC

      “IPAC--Inlet Performance Analysis Code” 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

      Online Access

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        4Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness

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        “Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Metadata:

        • Title: ➤  Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
        • Author:
        • Language: English
        • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
        • Publish Date:
        • Publish Location: ➤  Edwards, Calif - Springfield, VA

        “Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Subjects and Themes:

        Edition Identifiers:

        Access and General Info:

        • First Year Published: 2001
        • Is Full Text Available: No
        • Is The Book Public: No
        • Access Status: No_ebook

        Online Access

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          5International Space Station

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          “International Space Station” Metadata:

          • Title: International Space Station
          • Author:
          • Language: English
          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
          • Publish Date:
          • Publish Location: ➤  [Huntsville, Ala.] - Springfield, VA

          “International Space Station” Subjects and Themes:

          Edition Identifiers:

          Access and General Info:

          • First Year Published: 1998
          • Is Full Text Available: No
          • Is The Book Public: No
          • Access Status: No_ebook

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            6Flight test of an adaptive configuration optimization system for transport aircraft

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            “Flight test of an adaptive configuration optimization system for transport aircraft” Metadata:

            • Title: ➤  Flight test of an adaptive configuration optimization system for transport aircraft
            • Author:
            • Language: English
            • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
            • Publish Date:
            • Publish Location: ➤  [Springfield, Va - Edwards, Calif

            “Flight test of an adaptive configuration optimization system for transport aircraft” 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

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              7A Two element laminar flow airfoil optimized for cruise

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              “A Two element laminar flow airfoil optimized for cruise” Metadata:

              • Title: ➤  A Two element laminar flow airfoil optimized for cruise
              • Author:
              • Language: English
              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - Texas A&M University
              • Publish Date:
              • Publish Location: ➤  Springfield, Va - [Washington, DC - [College Station, TX?]

              “A Two element laminar flow airfoil optimized for cruise” Subjects and Themes:

              Edition Identifiers:

              Access and General Info:

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

              Online Access

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                8On the use of external burning to reduce aerospace vehicle transonic drag

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                “On the use of external burning to reduce aerospace vehicle transonic drag” Metadata:

                • Title: ➤  On the use of external burning to reduce aerospace vehicle transonic drag
                • Author:
                • Language: English
                • Number of Pages: Median: 14
                • Publisher: ➤  NASA - For sale by the National Technical Information Service
                • Publish Date:
                • Publish Location: ➤  [Washington, D.C.] - [Springfield, Va

                “On the use of external burning to reduce aerospace vehicle transonic drag” 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

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                  9Robust airfoil optimization to achieve consistent drag reduction over a mach range

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                  “Robust airfoil optimization to achieve consistent drag reduction over a mach range” Metadata:

                  • Title: ➤  Robust airfoil optimization to achieve consistent drag reduction over a mach range
                  • Author:
                  • Language: English
                  • Publisher: ➤  Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Langley Research Center
                  • Publish Date:
                  • Publish Location: Hampton, Va - Hanover, MD

                  “Robust airfoil optimization to achieve consistent drag reduction over a mach range” Subjects and Themes:

                  Edition Identifiers:

                  Access and General Info:

                  • First Year Published: 2001
                  • Is Full Text Available: No
                  • Is The Book Public: No
                  • Access Status: No_ebook

                  Online Access

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                    10A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept

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                    “A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Metadata:

                    • Title: ➤  A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
                    • Author:
                    • Language: English
                    • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                    • Publish Date:
                    • Publish Location: [Springfield, Va - Hampton, Va

                    “A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” 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

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                      11Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results

                      By

                      “Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Metadata:

                      • Title: ➤  Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
                      • Author:
                      • Language: English
                      • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                      • Publish Date:
                      • Publish Location: Hampton, Va - Springfield, VA

                      “Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” 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

                      Online Access

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                        12Study of potential aerodynamic benefits from spanwise blowing at wingtip

                        By

                        “Study of potential aerodynamic benefits from spanwise blowing at wingtip” Metadata:

                        • Title: ➤  Study of potential aerodynamic benefits from spanwise blowing at wingtip
                        • Author:
                        • Language: English
                        • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                        • Publish Date:
                        • Publish Location: Hampton, Va - [Springfield, Va

                        “Study of potential aerodynamic benefits from spanwise blowing at wingtip” 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

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                          13A novel potential viscous flow coupling technique for computing helicopter flow fields

                          By

                          “A novel potential viscous flow coupling technique for computing helicopter flow fields” Metadata:

                          • Title: ➤  A novel potential viscous flow coupling technique for computing helicopter flow fields
                          • Author:
                          • Language: English
                          • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center
                          • Publish Date:
                          • Publish Location: Moffett Field, Calif

                          “A novel potential viscous flow coupling technique for computing helicopter flow fields” 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:

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                            14Reducing wind tunnel data requirements using neural networks

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                            “Reducing wind tunnel data requirements using neural networks” Metadata:

                            • Title: ➤  Reducing wind tunnel data requirements using neural networks
                            • Author:
                            • Language: English
                            • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                            • Publish Date:
                            • Publish Location: ➤  Moffett Field, Calif - [Springfield, Va

                            “Reducing wind tunnel data requirements using neural networks” 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

                            Online Access

                            Downloads Are Not Available:

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                              15Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2

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                              “Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2” Metadata:

                              • Title: ➤  Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2
                              • Author:
                              • Number of Pages: Median: 46
                              • Publisher: [Institute of Aerophysics]
                              • Publish Date:
                              • Publish Location: [Downsview, Ont.]

                              “Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2” Subjects and Themes:

                              Edition Identifiers:

                              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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                              16Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2

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                              “Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2” Metadata:

                              • Title: ➤  Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2
                              • Author:
                              • Number of Pages: Median: 46
                              • Publisher: Institute of Aerophysics
                              • Publish Date:
                              • Publish Location: [Downsview, Ont.]

                              “Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2” Subjects and Themes:

                              Edition Identifiers:

                              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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                              17A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles

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                              “A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles” Metadata:

                              • Title: ➤  A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles
                              • Author:
                              • Number of Pages: Median: 19
                              • Publisher: ➤  National Research Council Canada, National Aeronautical Establishment
                              • Publish Date:
                              • Publish Location: Ottawa

                              “A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles” Subjects and Themes:

                              Edition Identifiers:

                              Access and General Info:

                              • First Year Published: 1973
                              • Is Full Text Available: No
                              • Is The Book Public: No
                              • Access Status: No_ebook

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                              18Analysis and evaluation of an integrated laminar flow control propulsion system

                              By

                              “Analysis and evaluation of an integrated laminar flow control propulsion system” Metadata:

                              • Title: ➤  Analysis and evaluation of an integrated laminar flow control propulsion system
                              • Author:
                              • Language: English
                              • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                              • Publish Date:
                              • Publish Location: ➤  Springfield, Va - [Washington, DC

                              “Analysis and evaluation of an integrated laminar flow control propulsion system” 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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                                19Control of oscillatory forces on a circular cylinder by rotation

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                                “Control of oscillatory forces on a circular cylinder by rotation” Metadata:

                                • Title: ➤  Control of oscillatory forces on a circular cylinder by rotation
                                • Author:
                                • Language: English
                                • Publisher: ➤  Institute for Computer Applications in Science and Enginering, NASA Langley Research Center - National Technical Information Service, distributor
                                • Publish Date:
                                • Publish Location: Hampton, Va - [Springfield, Va

                                “Control of oscillatory forces on a circular cylinder by rotation” 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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                                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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                                  20Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter

                                  By

                                  “Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter” Metadata:

                                  • Title: ➤  Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter
                                  • Author:
                                  • Language: English
                                  • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                  • Publish Date:
                                  • Publish Location: ➤  Washington, DC - [Springfield, Va

                                  “Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter” 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

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                                  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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                                    21High altitude towed glider

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                                    “High altitude towed glider” Metadata:

                                    • Title: High altitude towed glider
                                    • Author:
                                    • Language: English
                                    • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor
                                    • Publish Date:
                                    • Publish Location: ➤  [Washington, D.C - Springfield, Va

                                    “High altitude towed glider” 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

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                                      22A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program

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                                      “A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program” Metadata:

                                      • Title: ➤  A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program
                                      • Author:
                                      • Language: English
                                      • Publisher: ➤  National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
                                      • Publish Date:
                                      • Publish Location: ➤  Edwards, Calif - [Springfield, Va

                                      “A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program” 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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                                      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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                                        23A concept for adaptive performance optimization on commercial transport aircraft

                                        By

                                        “A concept for adaptive performance optimization on commercial transport aircraft” Metadata:

                                        • Title: ➤  A concept for adaptive performance optimization on commercial transport aircraft
                                        • Author:
                                        • Language: English
                                        • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor]
                                        • Publish Date:
                                        • Publish Location: ➤  Edwards, Calif - [Springfield, Va

                                        “A concept for adaptive performance optimization on commercial transport aircraft” 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

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                                          24A preliminary design study of supersonic through-flow fan inlets

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                                          “A preliminary design study of supersonic through-flow fan inlets” Metadata:

                                          • Title: ➤  A preliminary design study of supersonic through-flow fan inlets
                                          • Author:
                                          • Language: English
                                          • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                          • Publish Date:
                                          • Publish Location: ➤  [Springfield, Va - [Washington, D.C.]

                                          “A preliminary design study of supersonic through-flow fan inlets” Subjects and Themes:

                                          Edition Identifiers:

                                          Access and General Info:

                                          • First Year Published: 1988
                                          • 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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                                            25An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models

                                            By

                                            “An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models” Metadata:

                                            • Title: ➤  An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models
                                            • Author:
                                            • Language: English
                                            • Publisher: ➤  National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
                                            • Publish Date:
                                            • Publish Location: ➤  [Springfield, Va - Moffett Field, CA

                                            “An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models” 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

                                            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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                                              26Neural network prediction of new aircraft design coefficients

                                              By

                                              “Neural network prediction of new aircraft design coefficients” Metadata:

                                              • Title: ➤  Neural network prediction of new aircraft design coefficients
                                              • Author:
                                              • Language: English
                                              • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
                                              • Publish Date:
                                              • Publish Location: ➤  [Springfield, Va - Moffett Field, Calif

                                              “Neural network prediction of new aircraft design coefficients” 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

                                              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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                                                27Model engine performance measurement from force balance instrumentation

                                                By

                                                “Model engine performance measurement from force balance instrumentation” Metadata:

                                                • Title: ➤  Model engine performance measurement from force balance instrumentation
                                                • Author:
                                                • Language: English
                                                • Publisher: ➤  National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
                                                • Publish Date:
                                                • Publish Location: ➤  [Springfield, Va - [Cleveland, Ohio]

                                                “Model engine performance measurement from force balance instrumentation” Subjects and Themes:

                                                Edition Identifiers:

                                                Access and General Info:

                                                • First Year Published: 1998
                                                • Is Full Text Available: No
                                                • Is The Book Public: No
                                                • Access Status: No_ebook

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                                                  28A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies

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                                                  “A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies” Metadata:

                                                  • Title: ➤  A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies
                                                  • Author:
                                                  • Number of Pages: Median: 39
                                                  • Publisher: National Aerospace Laboratory
                                                  • Publish Date:
                                                  • Publish Location: Amsterdam

                                                  “A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies” 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

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                                                  29Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models

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                                                  “Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models” Metadata:

                                                  • Title: ➤  Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models
                                                  • Author:
                                                  • Number of Pages: Median: 14
                                                  • Publisher: ➤  College of Aeronautics, Cranfield Institute of Technology
                                                  • Publish Date:
                                                  • Publish Location: Cranfield, U.K

                                                  “Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models” 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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                                                  30A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme

                                                  By

                                                  “A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme” Metadata:

                                                  • Title: ➤  A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme
                                                  • Author:
                                                  • Number of Pages: Median: 25
                                                  • Publisher: ➤  College of Aeronautics, Cranfield Institute of Technology
                                                  • Publish Date:
                                                  • Publish Location: Cranfield [U.K.]

                                                  “A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme” Subjects and Themes:

                                                  Edition Identifiers:

                                                  Access and General Info:

                                                  • First Year Published: 1987
                                                  • Is Full Text Available: No
                                                  • Is The Book Public: No
                                                  • Access Status: No_ebook

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                                                  31Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?

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                                                  “Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” Metadata:

                                                  • Title: ➤  Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
                                                  • Author:
                                                  • Number of Pages: Median: 24
                                                  • Publisher: AGARD
                                                  • Publish Date:
                                                  • Publish Location: Neuilly sur Seine, France

                                                  “Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” 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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                                                  32A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept

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                                                  “A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept” Metadata:

                                                  • Title: ➤  A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
                                                  • Author:
                                                  • Language: English
                                                  • Publisher: ➤  National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
                                                  • Publish Date:
                                                  • Publish Location: Hampton, Va - [Springfield, Va

                                                  “A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept” Subjects and Themes:

                                                  Edition Identifiers:

                                                  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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                                                    33Aerodynamics of heat exchangers for high-altitude aircraft

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                                                    “Aerodynamics of heat exchangers for high-altitude aircraft” Metadata:

                                                    • Title: ➤  Aerodynamics of heat exchangers for high-altitude aircraft
                                                    • Author:
                                                    • Language: English
                                                    • Publisher: ➤  National Technical Information Service, distributor - National Aeronautics and Space Administration
                                                    • Publish Date:
                                                    • Publish Location: ➤  [Washington, DC - Springfield, Va

                                                    “Aerodynamics of heat exchangers for high-altitude aircraft” 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

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                                                      34Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D

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                                                      “Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D” Metadata:

                                                      • Title: ➤  Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D
                                                      • Author:
                                                      • Language: English
                                                      • Publisher: ➤  Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
                                                      • Publish Date:
                                                      • Publish Location: Hampton, Va - Hanover MD

                                                      “Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D” Subjects and Themes:

                                                      Edition Identifiers:

                                                      Access and General Info:

                                                      • First Year Published: 2001
                                                      • Is Full Text Available: No
                                                      • Is The Book Public: No
                                                      • Access Status: No_ebook

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                                                        35Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight

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                                                        “Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Metadata:

                                                        • Title: ➤  Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
                                                        • Author:
                                                        • Language: English
                                                        • Publisher: ➤  National Aeronautics and Space Administration - National Technical Information Service, distributor - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
                                                        • Publish Date:
                                                        • Publish Location: ➤  Springfield, Va - Boca Raton, FL - [Washington, DC

                                                        “Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Subjects and Themes:

                                                        Edition Identifiers:

                                                        Access and General Info:

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

                                                        Online Access

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                                                        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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                                                          36Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

                                                          By

                                                          “Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Metadata:

                                                          • Title: ➤  Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
                                                          • Author:
                                                          • Language: English
                                                          • Publisher: ➤  For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
                                                          • Publish Date:
                                                          • Publish Location: ➤  Springfield, Va - Washington, D.C

                                                          “Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” 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

                                                          Online Access

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                                                          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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                                                            37Demonstration of the coast-down technique for determining train resistances

                                                            By

                                                            “Demonstration of the coast-down technique for determining train resistances” Metadata:

                                                            • Title: ➤  Demonstration of the coast-down technique for determining train resistances
                                                            • Author:
                                                            • Language: English
                                                            • Publisher: ➤  National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology
                                                            • Publish Date:
                                                            • Publish Location: Pasadena, Calif

                                                            “Demonstration of the coast-down technique for determining train resistances” 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

                                                            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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