1984 …2019

Research output per year

If you made any changes in Pure these will be visible here soon.

Fingerprint Weighted list of dominant concepts in the researcher's publications (titles and abstracts).

Network Recent external collaboration on country level. Dive into details by clicking on the dots.

Research Output

Bow shock/vortex interaction: Effect of reducing the vortex height on structure of the generated flow field

Pourhashem, H. & Kumar, S., Jan 1 2019, AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics Inc, AIAA, (AIAA Scitech 2019 Forum).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • Flow Field Characteristics of a Supersonic Jet Influenced by Downstream Microjet Fluidic Injection

    Pourhashem, H. & Kumar, S., Oct 2019, In : Aerospace Science and Technology. 93, 105281.

    Research output: Contribution to journalArticle

  • Use of downstream fluid injection to reduce subsonic jet noise

    Rajput, P. & Kumar, S., Jul 1 2019, In : International Journal of Aeroacoustics. 18, 4-5, p. 554-574 21 p.

    Research output: Contribution to journalArticle

  • Design optimization of a single-mode microring resonator for label-free detection of biomarkers within a tunable spectral range of 2 nm

    Panindre, P., Susan Mousavi, N. & Kumar, S., Jan 1 2018, Biomedical Imaging and Sensing Conference. SPIE, Vol. 10711. 1071126

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

  • Directionally-targeted jet noise supression: Benefits of asymmetric downstream fluidic injection

    Rajput, P. & Kumar, S., Jan 1 2018, 2018 AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics Inc, AIAA, AIAA 2018-3609

    Research output: Chapter in Book/Report/Conference proceedingConference contribution