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  • Author > Cho, Y. I. [x]

  • Sort results by: NASA Center | Date Added to NTRS | Publication Year
    There are a total of 21 record(s) matching your query.
    Sorted by: Date Added To NTRS in Descending order

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    Fundamental study of flow field generated by rotorcraft blades using wide-field shadowgraph

    Author(s): Parthasarathy, S. P.; Cho, Y. I.; Back, L. H.
    Abstract: The vortex trajectory and vortex wake generated by helicopter rotors are visualized using a wide-field shadowgraph technique. Use of a retro-reflective Scotchlite screen makes it possible to investigate the flow field ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1985
    Added to NTRS: 2004-11-03
    Accession Number: 86N15249; Document ID: 19860005779; Report Number: JPL-PUB-85-64, NAS 1.26:176443, NASA-CR-176443

    Measurement of sound emitted by flying projectiles with aeroacoustic sources

    Author(s): Cho, Y. I.; Shakkottai, P.; Harstad, K. G.; Back, L. H.
    Abstract: Training projectiles with axisymmetric ring cavities that produce intense tones in an airstream were shot in a straight-line trajectory. A ground-based microphone was used to obtain the angular distribution of sound ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1988
    Added to NTRS: 2004-11-03
    Accession Number: 89A29305; Document ID: 19890041934

    Fluid particle motion and Lagrangian velocities for pulsatile flow through a femoral artery branch model

    Author(s): Cho, Y. I.; Crawford, D. W.; Back, L. H.; Back, M. R.
    Abstract: A flow visualization study using selective dye injection and frame by frame analysis of a movie provided qualitative and quantitative data on the motion of marked fluid particles in a 60 degree artery branch model for ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1987
    Added to NTRS: 2004-11-03
    Accession Number: 88A20310; Document ID: 19880033083

    Yaw and spin effects on high intensity sound generation and on drag of training projectiles with ring cavities

    Author(s): Parthasarathy, S. P.; Cho, Y. I.; Kwack, E. Y.; Back, L. H.
    Abstract: Projectiles containing axisymmetric ring cavities constitute aeroacoustic sources. These produce high intensity tones which are used for coding in the SAWE (Simulation of Area Weapons Effects) system. Experimental data ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1986
    Added to NTRS: 2004-11-03
    Accession Number: 86A19924; Document ID: 19860035186; Report Number: AIAA PAPER 86-0515

    Rain simulation studies for high-intensity acoustic nose cavities

    Author(s): Clayton, R. M.; Cho, Y. I.; Shakkottai, P.; Back, L. H.
    Abstract: Unarmed plastic projectiles can be equipped with small axisymmetric cavities for the generation of intense tones that are useful in training maneuvers. Attention is presently given to the simulation of rainfall in an ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1988
    Added to NTRS: 2004-11-03
    Accession Number: 88A45689; Document ID: 19880058462

    Aerodynamic sound generation induced by flow over small, cylindrical cavities

    Author(s): Parthasarathy, S. P.; Cho, Y. I.; Back, L. H.
    Abstract: An experimental investigation has been conducted on the production of high intensity tones by small cylindrical cavities in a flat surface. The application of such a mechanism is to the acoustic coding of moving objects ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1984
    Added to NTRS: 2004-11-03
    Accession Number: 85A10827; Document ID: 19850028676; Report Number: AIAA PAPER 84-2258

    Fluid dynamic study in a femoral artery branch casting of man with upstream main lumen curvature for steady flow

    Author(s): Cho, Y. I.; Back, L. H.; Back, M. R.
    Abstract: An in-vitro, steady flow investigation was conducted in a hollow, transparent vascular replica of the profunda femoris branch of man for a range of physiological flow conditions. The replica casting tested was obtained from ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1985
    Added to NTRS: 2004-11-03
    Accession Number: 86A45254; Document ID: 19860060516

    Measurement and prediction of flow through a replica segment of a mildly atherosclerotic coronary artery of man

    Author(s): Back, L. H.; Radbill, J. R.; Cho, Y. I.; Crawford, D. W.
    Abstract: Pressure distributions were measured along a hollow vascular axisymmetric replica of a segment of the left circumflex coronary artery of man with mildly atherosclerotic diffuse disease. A large range of physiological ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1986
    Added to NTRS: 2004-11-03
    Accession Number: 86A43440; Document ID: 19860058702

    Pool fires in a simulated aircraft cabin interior with ventilation

    Author(s): Bankston, C. P.; Back, L. H.; Cho, Y. I.; Shakkottai, P.
    Abstract: Results of experiments conducted at the JPL to evaluate aircraft postcrash fire hazards are presented. The experiments were carried out in a one-third scale simulated aircraft cabin geometry to study pool fire and ...
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1987
    Added to NTRS: 2004-11-03
    Accession Number: 87A53783; Document ID: 19870066509

    Experimental study of pulsatile and steady flow through a smooth tube and an atherosclerotic coronary artery casting of man

    Author(s): Cho, Y. I.; Back, L. H.; Cuffel, R. F.; Crawford, D. W.
    Abstract: No Abstract Available
    NASA Center: Jet Propulsion Laboratory
    Publication Year: 1983
    Added to NTRS: 2004-11-03
    Accession Number: 84A34962; Document ID: 19840052175

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