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Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / / Frank J. Kurtenbach and Frank W. Burcham, Jr
| Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane / / Frank J. Kurtenbach and Frank W. Burcham, Jr |
| Autore | Kurtenbach Frank J. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1981 |
| Descrizione fisica | 1 online resource (18 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Afterburning
F-15 aircraft Jet thrust Pressure measurement Turbofan engines Airplanes - Motors - Thrust Fighter planes - Turbojet engines Jet propulsion |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707439203321 |
Kurtenbach Frank J.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , January 1981 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Reduced and derated takeoff thrust (power) procedures [[electronic resource]]
| Reduced and derated takeoff thrust (power) procedures [[electronic resource]] |
| Pubbl/distr/stampa | [Washington, D.C.] : , : U.S. Dept. of Transportation, Federal Aviation Administration, , [1988] |
| Descrizione fisica | 4 pages : digital, PDF file |
| Collana | Advisory circular |
| Soggetto topico |
Airplanes - Takeoff
Airplanes - Motors - Thrust |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Reduced and derated takeoff thrust |
| Record Nr. | UNINA-9910697706203321 |
| [Washington, D.C.] : , : U.S. Dept. of Transportation, Federal Aviation Administration, , [1988] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles / / Mary L. Mason and Bobby L. Berrier
| Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles / / Mary L. Mason and Bobby L. Berrier |
| Autore | Mason Mary L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , June 1985 |
| Descrizione fisica | 1 online resource (216 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Static tests
Thrust vector control Convergent-divergent nozzles Yaw Wind tunnel tests Jet nozzles - Testing Yawing (Aerodynamics) Airplanes - Motors - Thrust |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709791903321 |
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Mason Mary L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , June 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability / / Mary L. Mason and James R. Burley II
| Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability / / Mary L. Mason and James R. Burley II |
| Autore | Mason Mary L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (54 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Nozzle geometry
Static tests Nozzle thrust coefficients Axisymmetric flow Afterburning Jet nozzles - Testing Airplanes - Motors - Thrust Pitching (Aerodynamics) Short take-off and landing aircraft |
| Soggetto genere / forma | Online resources. |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709724803321 |
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Mason Mary L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program / / Scott C. Asbury and Jeffrey A. Yetter
| Static performance of six innovative thrust reverser concepts for subsonic transport applications : summary of the NASA Langley Innovative Thrust Reverser Test Program / / Scott C. Asbury and Jeffrey A. Yetter |
| Autore | Asbury Scott C. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2000 |
| Descrizione fisica | 1 online resource (30 pages, 334 unnumbered pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Airplanes - Brakes
Airplanes - Design and construction Airplanes - Motors - Thrust Airplanes - Turbofan engines Jet planes - Thrust reversers - Testing Thrust reversal Turbofans Aeronautical engineering Aircraft design Performance tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Static performance of six innovative thrust reverser concepts for subsonic transport applications |
| Record Nr. | UNINA-9910707886903321 |
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Asbury Scott C.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Thrust and drag [[electronic resource] ] : its prediction and verification / / edited by Eugene E. Covert ; associate editors, C.R. James ... [et al.]
| Thrust and drag [[electronic resource] ] : its prediction and verification / / edited by Eugene E. Covert ; associate editors, C.R. James ... [et al.] |
| Pubbl/distr/stampa | New York, : American Institute of Aeronautics and Astronautics, c1985 |
| Descrizione fisica | 1 online resource (352 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
CovertEugene E
JamesC. R |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Drag (Aerodynamics)
Airplanes - Motors - Thrust |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-573-9
1-60086-354-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Introduction""; ""An Historic Perspective""; ""Performance Calculations""; ""Estimation and Prediction of Drag""; ""A Short History of the Turbojet Engine""; ""The Turbine""; ""Compressor""; ""Flight Validation""; ""Chapter II. Thrust-Drag Accounting Methodology""; ""Thrust-Drag Accounting Approach""; ""Airframe System Drag""; ""Flow-Through Model Internal Drag Correction""; ""Scale-Model/Full Scale Geometry Correction""; ""Trim Drag""; ""Reynolds Number Correction""; ""Full Scale Drag Polar""
""Engine Thrust""""Throttle-Dependent Drags""; ""Inlet Spillage Drag""; ""Exhaust System Drag""; ""Auxiliary Airflow Thrust Drag""; ""Net Propulsive Force""; ""Chapter III. Gas Turbine Engine Performance Determination""; ""Engine Performance Estimation by Analysis and Calculation""; ""Practical Computational Limitations""; ""General Application of Thermodynamic Approach""; ""The Need for Approximations and Correlations""; ""Thermal and Mechanical Equilibrium Considerations""; ""Nonuniform Flowfields""; ""Engine Computer Math Models""; ""Performance Estimation by Ground Testing"" ""Test Configurations""""Factors Affecting Engine Performance Measurement""; ""Measurement Schemes""; ""Measurement Error Sources""; ""Measurement Resource Estimating""; ""Measurement Validation""; ""Scale-Model Test Comparisons""; ""Short-Duration Turbine Engine Testing""; ""Engine Performance Estimation by Flight Testing""; ""Preflight Test Considerations""; ""Engine Installation Effects""; ""Engine Evaluation Methods""; ""Flight Instrumentation Considerations""; ""Unsteady Influences on Thrust Determination in Flight""; ""Calculational Considerations"" ""Chapter IV. Prediction and Verification of Aerodynamic Drag, Part I: Prediction""""Introduction""; ""Drag""; ""Level of Drag Prediction Detail""; ""Subsonic Drag""; ""Empirical Correlations""; ""Detailed Drag Estimates�Component Buildup""; ""Cruise Efficiency""; ""Transonic Drag""; ""The Drag Rise""; ""Detailed Drag Estimates�Component Buildup""; ""Numerical Transonic Aerodynamics""; ""Supersonic Drag""; ""Friction Drag""; ""Wave Drag""; ""Lift-Induced Drag""; ""Numerical Aerodynamics"" ""Prediction and Verification of Aerodynamic Drag, Part II: Wind-Tunnel/Flight Correlation of Lift, Drag, and Pitching Moment""""Chapter V. Throttle-Dependent Forces""; ""Basic Concepts and Examples""; ""Supersonic/Transonic Aircraft Inlets""; ""Supersonic/Transonic Aircraft Nozzles""; ""Other Tactical Aircraft Throttle-Dependent Forces""; ""Subsonic Aircraft Inlets/Nozzles""; ""Determination of Throttle-Dependent Forces""; ""Experimental Techniques""; ""Difficulties in Experimental Testing""; ""Qualitative Techniques to Assess Throttle-Dependent Forces""; ""Analytical Techniques"" ""Throttle-Dependent Forces in Flight"" |
| Record Nr. | UNINA-9910457941103321 |
| New York, : American Institute of Aeronautics and Astronautics, c1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Thrust and drag [[electronic resource] ] : its prediction and verification / / edited by Eugene E. Covert ; associate editors, C.R. James ... [et al.]
| Thrust and drag [[electronic resource] ] : its prediction and verification / / edited by Eugene E. Covert ; associate editors, C.R. James ... [et al.] |
| Pubbl/distr/stampa | New York, : American Institute of Aeronautics and Astronautics, c1985 |
| Descrizione fisica | 1 online resource (352 p.) |
| Disciplina | 629.1 s |
| Altri autori (Persone) |
CovertEugene E
JamesC. R |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Drag (Aerodynamics)
Airplanes - Motors - Thrust |
| ISBN |
1-60086-573-9
1-60086-354-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter I. Introduction""; ""An Historic Perspective""; ""Performance Calculations""; ""Estimation and Prediction of Drag""; ""A Short History of the Turbojet Engine""; ""The Turbine""; ""Compressor""; ""Flight Validation""; ""Chapter II. Thrust-Drag Accounting Methodology""; ""Thrust-Drag Accounting Approach""; ""Airframe System Drag""; ""Flow-Through Model Internal Drag Correction""; ""Scale-Model/Full Scale Geometry Correction""; ""Trim Drag""; ""Reynolds Number Correction""; ""Full Scale Drag Polar""
""Engine Thrust""""Throttle-Dependent Drags""; ""Inlet Spillage Drag""; ""Exhaust System Drag""; ""Auxiliary Airflow Thrust Drag""; ""Net Propulsive Force""; ""Chapter III. Gas Turbine Engine Performance Determination""; ""Engine Performance Estimation by Analysis and Calculation""; ""Practical Computational Limitations""; ""General Application of Thermodynamic Approach""; ""The Need for Approximations and Correlations""; ""Thermal and Mechanical Equilibrium Considerations""; ""Nonuniform Flowfields""; ""Engine Computer Math Models""; ""Performance Estimation by Ground Testing"" ""Test Configurations""""Factors Affecting Engine Performance Measurement""; ""Measurement Schemes""; ""Measurement Error Sources""; ""Measurement Resource Estimating""; ""Measurement Validation""; ""Scale-Model Test Comparisons""; ""Short-Duration Turbine Engine Testing""; ""Engine Performance Estimation by Flight Testing""; ""Preflight Test Considerations""; ""Engine Installation Effects""; ""Engine Evaluation Methods""; ""Flight Instrumentation Considerations""; ""Unsteady Influences on Thrust Determination in Flight""; ""Calculational Considerations"" ""Chapter IV. Prediction and Verification of Aerodynamic Drag, Part I: Prediction""""Introduction""; ""Drag""; ""Level of Drag Prediction Detail""; ""Subsonic Drag""; ""Empirical Correlations""; ""Detailed Drag Estimates�Component Buildup""; ""Cruise Efficiency""; ""Transonic Drag""; ""The Drag Rise""; ""Detailed Drag Estimates�Component Buildup""; ""Numerical Transonic Aerodynamics""; ""Supersonic Drag""; ""Friction Drag""; ""Wave Drag""; ""Lift-Induced Drag""; ""Numerical Aerodynamics"" ""Prediction and Verification of Aerodynamic Drag, Part II: Wind-Tunnel/Flight Correlation of Lift, Drag, and Pitching Moment""""Chapter V. Throttle-Dependent Forces""; ""Basic Concepts and Examples""; ""Supersonic/Transonic Aircraft Inlets""; ""Supersonic/Transonic Aircraft Nozzles""; ""Other Tactical Aircraft Throttle-Dependent Forces""; ""Subsonic Aircraft Inlets/Nozzles""; ""Determination of Throttle-Dependent Forces""; ""Experimental Techniques""; ""Difficulties in Experimental Testing""; ""Qualitative Techniques to Assess Throttle-Dependent Forces""; ""Analytical Techniques"" ""Throttle-Dependent Forces in Flight"" |
| Record Nr. | UNINA-9910781412903321 |
| New York, : American Institute of Aeronautics and Astronautics, c1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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