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3 edition of Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations found in the catalog.

Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations

Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations

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  • 9 Currently reading

Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va .
Written in English

    Subjects:
  • Waveriders.,
  • Hypersonic vehicles.,
  • Aerodynamic characteristics.,
  • Wind tunnel models.,
  • Wind tunnel tests.,
  • Mach number.,
  • Flow distribution.,
  • Computational fluid dynamics.

  • Edition Notes

    Other titlesAerodynamic characteristics of two waverider derived hypersonic cruise configurations.
    StatementCharles E. Cockrell, Jr. and Lawrence D. Huebner, Dennis B. Finley.
    SeriesNASA technical paper -- 3559.
    ContributionsHuebner, Lawrence D., Finley, Dennis B., Langley Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL18118011M

    AERODYNAMIC PERFORMANCE AND FLOW-FIELD CHARACTERISTICS OF TWO WAVERIDER-DERIVED HYPERSONIC CRUISE CONFIGURATIONS Charles E. Cockrell, Jr.* and Lawrence D. Huebner? NASA Langley Research Center, Hampton, VA Dennis B. Finley** Lockheed-Fort Worth Company, Fort Worth, TX Abstract The component integration of a class of hypersonic high-lift con Read: Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations | National Aeronautics and Space Administration NASA | ISBN: | Kostenloser Versand für alle Bücher mit Versand und Verkauf duch : Taschenbuch.

    Robert J. McGhee and William D. Beasley, Low-Speed Aerodynamic Characteristics of a Percent-Thick Airfoil Section Designed for General Aviation Applications, NASA TN D, December , pp. Robert J. Pegg and David A. Hilton, Comparison of Acoustic Performance of Five Muffler Configurations on a Small Helicopter, NASA TN D, May Journal of Aerospace Technology and Management is a techno-scientific publication serialized, edited, and published by the Institute of Aeronautics and Space (Instituto de Aeronáutica e Espaço-IAE).

    Config Aero Hypersonics - Free download as PDF File .pdf), Text File .txt) or read online for free.   Minimum weight passive insulation requirements for hypersonic cruise vehicles. NASA Technical Reports Server (NTRS) Ardema, M. D. Analytical solutions are derived for.


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Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations Download PDF EPUB FB2

Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations Charles E. Cockrell, Jr. and Lawrence D. Huebner Langley Research Center • Hampton, Virginia Dennis B. Finley Lockheed-Fort Worth Company • Fort Worth, Texas National Aeronautics and Space Administration Langley Research Center • Hampton, Virginia jet.

The aerodynamic performance and PAI benefits offered by waveriders have generated interest in their use for various hypersonic vehicle designs. The purpose of the current study was to examine the aerodynamic characteristics of two waverider -derived hyper-sonic cruise vehicles.

Therefore, the objectives of this study were Size: 1MB. Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations (NASA technical paper) [Cockrell, Charles E] on *FREE* shipping on qualifying offers.

Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations (NASA technical paper). Get this from a library. Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations.

[Charles E Cockrell; Lawrence D Huebner; Dennis B Finley; Langley Research Center.]. Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations [microform] / Charles E. Cockrell, Jr. and Lawrence D. Huebner, Dennis B.

Finley National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor Hampton, Va.: [Springfield, Va aerodynamic characteristics in the terms of recovery coefficient of total pressure and uniformity coefficient.

References Charles ll,J, ect. Aerodynamics Characteristics of Two Waverider-Derived Hypersoni-c Cruise Configurations. NASA-Technical-Paper Liu. Buy Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations (NASA technical paper) by Charles E Cockrell (ISBN:) from Amazon's Book Store.

Everyday low prices and free delivery on eligible : Charles E Cockrell. Free 2-day shipping. Buy Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations at Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations eBook: National Aeronautics and Space Administration NASA: : Kindle StoreAuthor: National Aeronautics and Space Administration NASA.

Aerodynamic characteristics research on wide-speed range waverider configuration Article in Science in China Series E Technological Sciences 52(10) October with 18 Reads. Summary. A waverider configuration named DLR-F8 has been investigated in incompressible flow both experimentally and numerically.

A complex vortex system with primary, secondary and fuselage vortex has been found and a strong interaction between fuselage and primary vortex : R. Blaschke, D. Hummel. Hypersonic I-shaped aerodynamic configurations Article (PDF Available) in Science China: Physics, Mechanics and Astronomy 61(2) February with Reads How we measure 'reads'.

Cockrell, Charles E. and Huebner, Lawrence D. Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations, NASA TP, Cockrell, Charles E., Huebner, Lawrence D, and Finley, Dennis B. Aerodynamic Performance and Flow-Field Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations, AIAA Paper Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations [microform] / Char Numerical simulation of hypersonic aerodynamics and the computational needs for the design of an aerospa Effect of modifications on aerodynamic characteristics of a.

M. Lobbia, in Optimization of waverider-derived crew reentry vehicles using a rapid aerodynamics analysis approach: Proceedings of the 53rd AIAA Aerospace Sciences Meeting, (Kissimmee, Florida, ). Google ScholarCited by: 5. A suitable aerodynamic configuration for the gliding–cruising ballistic flight concept was analyzed.

• A new design concept, namely a gliding–cruising dual waverider, was proposed. • This methodology proposed is useful to design a hypersonic vehicle for two regimes of by: American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Hypersonic I-shaped aerodynamic configurations.

Kai Cui 1,2,*, Yao Xiao 1,2 The Aerodynamic Design of Aircraft (AIAA Inc., Blacksburg [7] M. Lobbia, in Optimization of waverider-derived crew reentry vehicles using a rapid aerodynamics analysis approach: Proceedings of the 53rd AIAA Aerospace Sciences Meeting, (Kissimmee Cited by: 5.

Figure 2: Hypersonic airplane based on waverider theory Air-Breathing Engines. The propulsion system for hypersonic speeds is a scramjet (= supersonic combustion ram jet), that is a system without moving parts.

(A recent review of scramjet technology is available in Curran-Heiser-Pratt, ). Experimental results of a Mach 10 conical-fl ow derived waverider to X hypersonic aerospace vehicle J. Manag., São José dos Campos, Vol.3, No.2, pp.May-Aug., edge, the supersonic fl ow streamlines are traced back until they reach the.

studies. A hypersonic vehicle configuration with waverider derived wings is shown in Figure 7. It is composed of an inlet as main body and two star-shaped geometries as wings and this work was done in subroutine inlet.

A total of three shockwaves are attached to this vehicle. Besides the added lift, the wings provide more volume to the entire.The conceptual aircraft design and its integration with a combined cycle engine for hypersonic cruise at Mach 8 is documented in this paper. The paper describes the process taken to develop a hypersonic aircraft from a conceptual approach.

The discussion also includes the design and CFD analysis of the integrated combined cycle engine. A final conceptual hypersonic transport aircraft with an Cited by: 2.1. Introduction. There has been a renewed interest in the waverider design due to recent military as well as other projects focusing on hypersonic conceived by Nonweiler, waverider is a lifting body that is derived from a known analytical flowfield such as flow over a two-dimensional wedge or flow around a slender term ‘waverider’ is used to describe a geometry Cited by: