YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    Search 
    •   YE&T Library
    • Search
    •   YE&T Library
    • Search
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Search

    Show Advanced FiltersHide Advanced Filters

    Filters

    Use filters to refine the search results.

    Now showing items 1-6 of 6

    • Relevance
    • Title Asc
    • Title Desc
    • Year Asc
    • Year Desc
    • 5
    • 10
    • 20
    • 40
    • 60
    • 80
    • 100
  • Export
    • CSV
    • RIS
    • Sort Options:
    • Relevance
    • Title Asc
    • Title Desc
    • Issue Date Asc
    • Issue Date Desc
    • Results Per Page:
    • 5
    • 10
    • 20
    • 40
    • 60
    • 80
    • 100

    Alterations in Critical Radii of Bluntness of Shock Wave Boundary Layer Interaction 

    Source: Journal of Aerospace Engineering:;2017:;Volume ( 030 ):;issue: 005
    Author(s): Bibin John; Vinayak Kulkarni
    Publisher: American Society of Civil Engineers
    Abstract: Any configuration consisting of flat plate attached to a ramp experiences shock wave boundary layer interaction (SWBLI) at supersonic or hypersonic Mach numbers. This interaction can lead to flow separation at the ramp ...
    Request PDF

    Accelerometer-Based Force Balance for High Enthalpy Facilities 

    Source: Journal of Aerospace Engineering:;2010:;Volume ( 023 ):;issue: 004
    Author(s): Vinayak Kulkarni; K. P. J. Reddy
    Publisher: American Society of Civil Engineers
    Abstract: A single component accelerometer-based force balance is developed, calibrated, and used for high enthalpy applications. Functionality of this force balance, for such applications, is demonstrated for the first time during ...
    Request PDF

    Delusive Influence of Nondimensional Numbers in Canonical Hypersonic Nonequilibrium Flows 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 005
    Author(s): Siddesh Desai; Vinayak Kulkarni; Hrishikesh Gadgil
    Publisher: American Society of Civil Engineers
    Abstract: A finite volume–based unstructured inviscid flow solver has been developed for the study of nonequilibrium effects in high enthalpy flows. Four different inviscid flux computation schemes are tested for literature reported ...
    Request PDF

    Experimental Exploration of Bioinspired Planar Wingtip Devices for a Flat-Plate Wing in the Low Reynolds Number Regime 

    Source: Journal of Aerospace Engineering:;2024:;Volume ( 037 ):;issue: 006:;page 04024075-1
    Author(s): Bastav Borah; Anand Verma; Vinayak Kulkarni; Ujjwal K. Saha
    Publisher: American Society of Civil Engineers
    Abstract: This study investigates the use of planar wingtip attachments to improve the lift generating performance of low aspect ratio (AR) flat-plate wings in the low Reynolds number (Re) range (<105). Inspired by nature’s ...
    Request PDF

    Laser Based Calibration Technique of Thin Film Gauges for Short Duration Transient Measurements 

    Source: Journal of Thermal Science and Engineering Applications:;2011:;volume( 003 ):;issue: 004:;page 44504
    Author(s): Rakesh Kumar; Niranjan Sahoo; Vinayak Kulkarni; Anugrah Singh
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Surface temperature history and determination of convective heating rate are the important activity in many research programs for devising an effective cooling system in internal combustion engines ...
    Request PDF

    Aerothermodynamic Assessment of Spiked Configuration for Drag Reduction at Hypersonic Speeds 

    Source: Journal of Aerospace Engineering:;2020:;Volume ( 033 ):;issue: 006
    Author(s): Shailendra Kumar; Vinayak Kulkarni; Satya Pramod Jammy
    Publisher: ASCE
    Abstract: Aerothermodynamic analysis was performed for blunt-body configurations with spikes mounted to determine drag reduction effectiveness. In-house perfect gas and chemical nonequilibrium solvers were utilized. The analysis ...
    Request PDF
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     

    Author

    ... View More

    Publisher

    Year

    Type

    Content Type

    Publication Title

    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian