Last edited by Mikall
Sunday, July 26, 2020 | History

4 edition of Five-hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel found in the catalog.

Five-hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel

Five-hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel

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  • 10 Currently reading

Published by National Aeronautics and Space Administration, Glenn Research Center, National Technical Information Service, distributor in [Cleveland, Ohio], [Springfield, Va .
Written in English

    Subjects:
  • Calibrating,
  • Data acquisition,
  • Free jets,
  • Ice formation,
  • Regression analysis,
  • Flow measurement

  • Edition Notes

    Other titlesFive hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel.
    StatementJose C. Gonsalez and E. Allen Arrington.
    Series[NASA contractor report] -- NASA/CR-1999-202330., NASA contractor report -- NASA CR-202330.
    ContributionsArrington, E. Allen., NASA Glenn Research Center.
    The Physical Object
    FormatMicroform
    Pagination1 v.
    ID Numbers
    Open LibraryOL17591423M
    OCLC/WorldCa42587324


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Five-hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel Download PDF EPUB FB2

Five-hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel. [Cleveland, Ohio]: [Springfield, Va: National Aeronautics and Space Administration, Glenn Research Center ; National Technical Information Service, distributor.

MLA Citation. Gonsalez, Jose C. and Arrington, E. Allen. and NASA Glenn Research Center. Get this from a library. Five-hole flow angle probe calibration for the NASA Glenn Icing Research Tunnel.

[Jose C Gonsalez; E Allen Arrington; NASA Glenn Research Center.]. pengukuran turbulensi dan angularitas aliran pada terowongan angin subsonik lapan (the measurement of turbulence and flow angularity in lapan’s subsonic wind tunnel). A spring test section calibration program is scheduled for the NASA Glenn Research Center Icing Research Tunnel following the installation of new water injecting spray bars.

Modification of Axial Fan Flow by Trailing Edge Self-Induced Blowing Matjaž Eberlinc, Matjaž Eberlinc. Five-Hole Flow Angle Probe Calibration for the NASA Glenn Icing Research Tunnel, Dynacs Engineering Company, Inc., Brook Park, by: 5. Flow visualization and wake analysis for complex three-dimensional bluff bodies at subcritical through critical Reynolds numbers Performance of the Phase Doppler Particle Analyzer icing cloud droplet sizing probe in the NASA Lewis Icing Research Tunnel.

RUDOFF, E. BACHALO, W. BACHALO A miniature fast-response five-hole probe for. Library of Congress Cataloging-in-Publication Data (Revised for vol. 8) NASA historical data book. (NASA SP- ) Vol. 1 is a republication of NASA historical data book, –/ Jane Van Nimmen and Leonard C.

Bruno. Vol. 8 in series: The NASA historical data book series. Includes bibliographical references and indexes. This banner text can have markup. web; books; video; audio; software; images; Toggle navigation.

NASA Images Solar System Collection Ames Research Center. Brooklyn Museum. Full text of "Aeronautical Engineering: A Continuing Bibliography With Indexes". NASA Historical Data Book Vol. 8 - Free ebook download as PDF File .pdf), Text File .txt) or read book online for free.

NASA earth science and space applications, aeronautics,technology and exploration, tracking and data acquisition/space operations, facilities and 5/5(1). Calibration of a pitot-static rake. NASA Technical Reports Server (NTRS) Stump, H. A five-element pitot-static rake was tested to confirm its accuracy and determine its suitability for use at Langley during low-speed tunnel calibration primarily at full-scale rake was tested at one airspeed of 74 miles per hour (33 meters per second) and at pitch and yaw.

ABOUT THE COVER: Left: Artist’s concept of Ares I on launch pad. NASA Glenn is designing and testing key subsystems of the upper stage for the Ares I Crew Launch Vehicle and is developing and manufacturing the Ares I–X Upper Stage Simulator test vehicle that will help prove the viability of the new rocket.

Look for Research & Technology for updates on this work. The Oxford Probe: an open access five-hole probe for aerodynamic measurements. NASA Astrophysics Data System (ADS) Hall, B.

F.; Povey, T. The Oxford Probe is an open access five-hole probe designed for experimental aerodynamic measurements. The open access probe can be manufactured by the end user via additive. Free essays, homework help, flashcards, research papers, book reports, term papers, history, science, politics.

Studylib. Documents Flashcards Grammar checker Login Upload document Create flashcards × Login Documents KSME International Journal, Vol. NASA Images Solar System Collection Ames Research Center. Brooklyn Museum.

Full text of "NASA Technical Reports Server (NTRS) Aeronautical engineering: A continuing bibliography with indexes (supplement )". The flow fields were surveyed by means of a five hole pressure probe at zero angle of attack. The test was performed at a free stream speed of 50 m/s with a thrust coefficient () and at advance ratio J = corresponding to a rather high power condition.

Richard T. Whitcomb with area-ruled F aircraft (NASA ) at the retirement of NASA (used for flight research at NASA Glenn and NASA Langley) at Langley in in the region of the wing; thereby the abrupt bump was avoided in area distribution. This approach resulted in a pronounced “wasp-waist” or “Coke-bottle” fuselage shape.5/5(3).

RED DEER ADVOCATE Friday, Nov. 28, A11 one of the challenges in courting new tenants is that many are years away from becoming operational. That won’t help fill the temporary void left by.