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Journal of Flow Visualization and Image Processing

Publication de 4  numéros par an

ISSN Imprimer: 1065-3090

ISSN En ligne: 1940-4336

The Impact Factor measures the average number of citations received in a particular year by papers published in the journal during the two preceding years. 2017 Journal Citation Reports (Clarivate Analytics, 2018) IF: 0.6 The Immediacy Index is the average number of times an article is cited in the year it is published. The journal Immediacy Index indicates how quickly articles in a journal are cited. Immediacy Index: 0.6 The Eigenfactor score, developed by Jevin West and Carl Bergstrom at the University of Washington, is a rating of the total importance of a scientific journal. Journals are rated according to the number of incoming citations, with citations from highly ranked journals weighted to make a larger contribution to the eigenfactor than those from poorly ranked journals. Eigenfactor: 0.00013 The Journal Citation Indicator (JCI) is a single measurement of the field-normalized citation impact of journals in the Web of Science Core Collection across disciplines. The key words here are that the metric is normalized and cross-disciplinary. JCI: 0.14 SJR: 0.201 SNIP: 0.313 CiteScore™:: 1.2 H-Index: 13

Indexed in

ELECTRICAL DISCHARGE TECHNIQUE FOR THREE-DIMENSIONAL FLOW FIELD VISUALIZATION IN HYPERSONIC SHOCK TUNNEL

Volume 4, Numéro 1, 1997, pp. 51-57
DOI: 10.1615/JFlowVisImageProc.v4.i1.50
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RÉSUMÉ

Visualization of flow around the bodies in a hypersonic shock tunnel based on electrical discharge is described. The flowfields around a flat plate with a sharp and blunt leading edge and a slender cone with sharp nose cone in HST1 shock tunnel at Mach 5.75 are visualized using this technique. The results of these studies are presented here. This technique can be extended for three-dimensional flow visualization by appropriate arrangement of the electrodes and the camera position.

CITÉ PAR
  1. Jagadeesh Gopalan, Nagashetty Kanderpallt, Reddy K. P. Jaganntha, Sun Mingyu, Takayama Kazuyoshi, Studies on the Effects of Test Gas on the Flow Field around Large Angle Blunt Cone Flying at Hypersonic Mach Number., TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 45, 149, 2002. Crossref

  2. Menezes Viren, Saravanan S., Jagadeesh G., Reddy K. P. J., Experimental Investigations of Hypersonic Flow over Highly Blunted Cones with Aerospikes, AIAA Journal, 41, 10, 2003. Crossref

  3. Menezes Viren, Saravanan S., Jagadeesh G., Reddy K. P. J, Aerodynamic Drag Reduction Using Aerospikes for Large Angle Blunt Cone Flying at Hypersonic Mach Number, 22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2002. Crossref

  4. Jagadeesh G., Sun M., Nagashetty K., Reddy K., Experimental investigations of test gas effects on the hypersonic flow field around large angle blunt cone in shock tunnel, 39th Aerospace Sciences Meeting and Exhibit, 2001. Crossref

  5. Mursenkova I V, Znamenskaya I A, Lutsky A E, Influence of shock waves from plasma actuators on transonic and supersonic airflow, Journal of Physics D: Applied Physics, 51, 10, 2018. Crossref

  6. Sriram Rengarajan, Jagadeesh Gopalan, Shock Tunnels and Hypersonic Research in IISc, Bangalore, in Experimental Methods of Shock Wave Research, 2016. Crossref

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