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title: aircraft aerodynamics design

Synonyme wurden verwendet für: Aircraft • Design
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    Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft

    Herrmann, U. | Tema Archiv | 2006
    focuses on the aerodynamic design of low-drag SCT high-lift systems contributing significant low-speed noise reductions by enabling steeper ...
    Schlagwörter: Luftfahrzeug

    Component-Based Model for Aerodynamic Noise of High-Speed Trains

    Iglesias, E.L. / Thompson, D.J. / Smith, M.G. | British Library Conference Proceedings | 2015

    Empirical Modeling of Railway Aerodynamic Noise Using One Microphone Pass-By Recording

    Zhang, X. | British Library Conference Proceedings | 2015

    Overview and History of Aircraft Inerting Systems

    SAE Technical Papers | 2021
    Aerospace Information Report (AIR) deals with the three methods of fuel tank inerting systems currently used in operational aircraft: (1) on-board ...
    Schlagwörter: Military aircraft , Commercial aircraft

    Aerodynamic Noise Reduction of a Pantograph Panhead by Applying a Flow Control Method

    Mitsumoji, T. / Sueki, T. / Yamazaki, N. et al. | British Library Conference Proceedings | 2015

    Analysis of Aerodynamic and Aeroacoustic Behaviour of a Simplified High-Speed Train Bogie

    Zhu, J.Y. / Hu, Z.W. / Thompson, D.J. | British Library Conference Proceedings | 2015

    SFB 880. Fundamentals of high-lift for future commercial aircraft

    Radespiel, Rolf / Semaan, Richard / Faßmann, B. et al. | Tema Archiv | 2013
    aircraft with active high lift system. (15) Structural design and aeroelasticity of circulation controlled wing. (16) An aircraft design with ...

    Aerodynamic performance of acoustically suppressed exhaust nozzles

    Wagenknecht, C.D. / Bediako, E. | Tema Archiv | 1984
    aircraft. This paper presents results of design studies, mission analysis, and scale model testing aimed at establishing a candidate AST exhaust ...

    Nasa Aircraft Controls Research, 1983

    G. P. Beasley | NTIS | 1984
    Schlagwörter: Aircraft , Aircraft design , Aircraft guidance , Aerodynamic stability , Structural design criteria

    Concept for Measuring Aeroacoustic Noise Transmission in Trains Derived from Experience Gained in Aircraft Testing

    Galuba, J. / Spehr, C. | British Library Conference Proceedings | 2015

    Application of advanced technology to future long-range aircraft

    Schrader, O. E. | NTRS | 1976
    incorporated advanced technology into the design of long-range passenger and cargo aircraft. The first technology centers around the use of an span ...
    Schlagwörter: Aircraft Design, Testing And Performance

    Aircraft engine noise quantities, noise sources and alleviation

    Jacques, R. | Tema Archiv | 1994
    This paper provides an overview of the aircraft noise. The classical noise units and these appropriate to quantify the annoyance related to ...

    Fan noise reduction from a supersonic inlet during simulated aircraft approach

    Nuckolls, W.E. / Ng, W.F. | Tema Archiv | 1993
    simulator noise source to that of a real aircraft engine on approach. Both aerodynamic and acoustic measurements were taken in the experiments. The ...
    Schlagwörter: Luftfahrzeug

    Aerodynamic Characteristics of the 10-Percent-Thick NASA Supercritical Airfoil 33 Designed for a Normal-Force Coefficient of 0.7

    C. D. Harris | NTIS | 1975
    A 10-percent-thick supercritical airfoil based on an off-design sonic-pressure plateau criterion was developed and experimental aerodynamic ...
    Schlagwörter: Aircraft , Aerodynamic characteristics , Aerodynamic coefficients

    Impact of rotor design on coaxial rotor performance, wake geometry and noise

    Wachspress, Daniel A. / Quackenbush, Todd R. | Tema Archiv | 2006
    Extensive research and development is currently underway to design next generation coaxial main rotor systems for heavy lift, high speed ...

    Design and testing of an active constrained layer damping demonstrator for aircraft's cabin noise reduction

    Vigliotti, Andrea / Sorrentino, Assunta | Tema Archiv | 2009
    to control. The most important noise path to aircrafts cabin is through fuselage panels. Through their vibration in fact both aerodynamic ...

    NASA CPAS Drogue Textile Riser Feasibility Study

    Hennings, Elsa J. / Petersen, Michael L. / Anderson, Brian et al. | NTRS | 2015
    design capable of protecting the riser against severe riser/crew module contact interactions. A feasibility study was then conducted to evaluate ...
    Schlagwörter: Aircraft Design, Testing And Performance

    Recent Advances in Structures for Hypersonic Flight, Part 1

    NTIS | 1978
    Schlagwörter: Aircraft , Aircraft design , Aircraft structures , Hypersonic aircraft , Structural design , Aerodynamic heating , Engine design

    Minimum Energy, Liquid Hydrogen Supersonic Cruise Vehicle Study

    G. D. Brewer / R. E. Morris | NTIS | 1975
    restriction on their design and operating performance. The baseline designs of LH2 fueled aircraft were than compared with equivalent designs of jet A ...
    Schlagwörter: Aircraft , Supersonic aircraft , Aircraft design , Aircraft performance

    Energy Consumption Characteristics of Transports Using the Prop-Fan Concept

    NTIS | 1976
    airplanes designed for 3333.6 km range, 180 passengers, and Mach 0.8 cruise. A fuel saving of 9.7% at the design range was estimated for a prop-fan ...
    Verlag: Boeing Commercial Airplane Co., Seattle, Wash. Dept. of Preliminary Design
    Schlagwörter: Aircraft , Transport aircraft , Aerodynamic drag

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