6,795 research outputs found

    Evaluative criteria for health education at the elementary school level

    Full text link
    Thesis (Ed.M.)--Boston Universit

    Instrument for use in performing a controlled Valsalva maneuver Patent

    Get PDF
    Piston device for producing known constant positive pressure within lungs by using thoracic muscle

    U.S EEOC v. Lakemont Homes, et al.

    Get PDF

    U.S. EEOC v. Lakemont Homes, Inc.

    Get PDF

    Remarks on imperfections of axially loaded cylinders

    Get PDF
    Imperfections of axially loaded cylindrical shell

    Volatile metal deposits on lunar soils: Relation to volcanism

    Get PDF
    Parallel leaching and volatilization experiments conducted on lunar samples and similar experiments on sphalerite do not supply the information needed to resolve the question of the chemical nature of pb 204, Zn, Bi and Tl deposits on lunar soil surfaces. It is proposed that in Apollo 17 mare and terra soils and fractions of pb 204, Zn and Tl that are insoluble under mild, hot pH 5HNO3, leaching conditions and involatile at 600 C were originally surface deposits which became immobilized by migration into the silicate substrate or by chemisorption. Only Bi is predominantly indigenous. The implication is also that the soils over their respective times of evolution were exposed to heavy metal vapors or that an episodic exposure occurred after they had evolved. A sequence of events is proposed to account for orange 74220 and black 74001 glasses by lava fountaining and for soil 74241 as tephra from an explosive volcanic eruption

    The application of a numerical integration procedure developed by erwin fehlberg to the restricted problem of three bodies

    Get PDF
    Application of numerical integration procedures to restricted three-body proble

    Passive control of wing/store flutter

    Get PDF
    Results are presented for a passive flutter suppression approach known as the decoupler pylon. The decoupler pylon dynamically isolates the wing from store pitch inertia effects by means of soft spring/damper elements assisted by a low frequency feedback control system which minimizes static pitch deflections of the store because of maneuvers and changing flight conditions. Wind tunnel tests and analyses show that this relatively simple pylon suspension system provides substantial increases in flutter speed and reduces the sensitivity of flutter to changes in store inertia and center of gravity. Flutter characteristics of F-16 and YF-17 flutter models equipped with decoupler pylon mounted stores are presented and compared with results obtained on the same model configuration with active flutter suppression systems. These studies show both passive and active concepts to be effective in suppressing wing/store flutter. Also presented are data showing the influence of pylon stiffness nonlinearities on wing/store flutter
    corecore