Computational and Experimental Investigation of Subsonic Flow over a Sawtooth Notched Delta Wing

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Year: 2026

Institution: Amity Institute of Aerospace Engineering, Amity University Uttar Pradesh, Noida

Authors: Jayanta Sinha, J. K. Jain, Sadaf Rakhshan, Mihika Gupta, Alexandra Arnold Massey

Type: Research paper

Field: Aerospace Engineering, Aerodynamics

Methodology: Computational Fluid Dynamics (CFD), Experimental wind tunnel testing, Oil flow visualization

Aircraft component studied: Sawtooth delta wing

Test conditions: Subsonic flow at 21 m/s, angles of attack from -5° to 15°

Data recorded: Static pressure distribution, pressure coefficients, vortex formation

Comparative analysis: Simple delta wing vs sawtooth delta wing

Objective: Analyze vortex lift and flow characteristics at low subsonic speeds

Publication format: Academic journal article

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CLES Generic Notched Marking Criteria for the 2016/17 Academic Session

Year: 2016/17

Institution: College of Life and Environmental Sciences, University of Exeter

Type: Assessment Guidelines

Audience: Undergraduate and Postgraduate Students

Scope: All taught programmes across disciplines and levels

Reference: University Teaching Quality Assurance Manual (TQA)

Levels Covered: Level 3 (pre-UG), Level 4 (first year UG), Level 5 (second year UG), Level 6 (final year UG), Level 7 (Masters)

Assessment Method: Subjective marking, excluding MCQ, SAQ, or national criteria-based assessments

Topics: Subsonic Sawtooth Notched

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