2,460 research outputs found

    Development of SCR Aircraft takeoff and landing procedures for community noise abatement and their impact on flight safety

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    Piloted simulator studies to determine takeoff and landing procedures for a supersonic cruise transport concept that result in predicted community noise levels which meet current Federal Aviation Administration (FAA) standards are discussed. The results indicate that with the use of advanced procedures, the subject simulated aircraft meets the FAA traded noise levels during takeoff and landing utilizing average flight crew skills. The advanced takeoff procedures developed involved violating three of the current Federal Aviation Regulations (FAR) noise test conditions. These were: (1) thrust cutbacks at altitudes below 214 meters (700 ft); (2) thrust cutback level below those presently allowed; and (3) configuration change, other than raising the landing gear. It was not necessary to violate any FAR noise test conditions during landing approach. It was determined that the advanced procedures developed do not compromise flight safety. Automation of some of the aircraft functions reduced pilot workload, and the development of a simple head-up display to assist in the takeoff flight mode proved to be adequate

    Analytical study of effects of severe turbulence on flight motions of a typical subsonic jet-transport airplane

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    Atmospheric turbulence effects on stability and response characteristics of subsonic jet transport aircraf

    Birds of Alas Purwo National Park, East Java

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    This paper details some of the more important and interesting records from Alas Purwo National Park in East Java. Most of these come from the author's work in the Park from May 1997 until September 1999, though records are included from many other sources. Details are given of the status of all of the species that are classed as threatened or near-threatened by Collar et al. (1994), along with those that are attitudinally or distributionally unexpected. A full systematic list of the species recorded in and around the Park is included, some 227 to date (with an additional 11 'possible' species)

    Australian Pelican in East Timor, an armchair record

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    Record of Hardhead (white-eyed Duck) from Lombok

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    Matsudaira's Storm-Petrel second record for the Lombok Strait

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    Lesser Adjutant breeding in Alas Purwo National Park, East Java

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    A simulator study for the development and evaluation of operating procedures on a supersonic cruise research transport to minimize airport-community noise

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    Piloted-simulator studies were conducted to determine takeoff and landing operating procedures for a supersonic cruise research transport concept that result in predicted noise levels which meet current Federal Aviation Administration (FAA) certification standards. With the use of standard FAA noise certification test procedures, the subject simulated aircraft did not meet the FAA traded-noise-level standards during takeoff and landing. However, with the use of advanced procedures, this aircraft meets the traded-noise-level standards for flight crews with average skills. The advanced takeoff procedures developed involved violating some of the current Federal Aviation Regulations (FAR), but it was not necessary to violate any FAR noise-test conditions during landing approach. Noise contours were also determined for some of the simulated takeoffs and landings in order to indicate the noise-reduction advantages of using operational procedures other than standard

    Simulator study of the low-speed handling qualities of a supersonic cruise arrow-wing transport configuration during approach and landing

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    A fixed-based simulator study was conducted to determine the low-speed flight characteristics of an advanced supersonic cruise transport having an arrow wing, a horizontal tail, and four dry turbojets with variable geometry turbines. The primary piloting task was the approach and landing. The statically unstable (longitudinally) subject configuration has unacceptable low-speed handling qualities with no augmentation. Therefore, a hardened stability augmentation system is required to achieve acceptable handling qualities, should the normal operational stability and control augmentation system fail. In order to achieve satisfactory handling qualities, considerable augmentation was required
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