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1Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the hypersonic arbitrary-body program

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“Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the hypersonic arbitrary-body program” Metadata:

  • Title: ➤  Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the hypersonic arbitrary-body program
  • Author:
  • Language: English
  • Publisher: ➤  Langley Research Center - For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
  • Publish Date:
  • Publish Location: ➤  Hampton, Va - [Springfield, Va - [Washington, DC]

“Improved tangent-cone method for the Aerodynamic Preliminary Analysis System (APAS) version of the hypersonic arbitrary-body program” 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

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    in the initial safety analysis document. Due to the amount of trim the system applies to the horizontal stabilizer, aerodynamic forces resist pilot control

    Baldwin Mono Tiltrotor

    Wayback Machine Baldwin, G. D., 'Preliminary Design Studies of a Mono Tiltrotor (MTR) with Demonstrations of Aerodynamic Wing Deployment', AHS International

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    February 1961 NASA awarded MIT a contract for preliminary design study of a guidance and navigation system for the Apollo program. MIT and the Delco Electronics

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    However, panel codes are still used for preliminary aerodynamic analysis as the time required for an analysis run is significantly less due to a decreased

    Multidisciplinary design optimization

    the conceptual and preliminary design stages. The disciplines considered in the BWB design are aerodynamics, structural analysis, propulsion, control

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    only while considering the coupled aerodynamic and structural system that requires rigorous mathematical analysis to reveal all the degrees of freedom

    Atmospheric entry

    Mission Analysis Tool (AMAT) provides preliminary mission analysis and simulation capability for atmospheric entry vehicles at various Solar System destinations

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    NASA Software of the Year Award. Cart3D is a high-fidelity analysis package for aerodynamic design which allows users to perform automated CFD simulations

    Phalanx CIWS

    rounds are designed to destroy a missile's airframe and make it non-aerodynamic, thus keeping shrapnel from the exploding projectile to a minimum, effectively


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