most citedTurbojet Module Sizing for Integration with Turbine-Based Combined Cycle Engine

1 citations · 2 across the 4 of their papers we have counts for

collaborators
Showing physics.flu-dynShow all

5 papers · 1 filter

physics.flu-dyn2025

Aerodynamic Design Considerations for Biconic Supersonic Air Intakes Revisited

J. P. S. Sandhu, M. Bhardwaj, N. Ananthkrishnan +4

Traditional design principles for determining the optimal intake ramp or cone angles, for ensuring no flow spillage at the intake cowl under design conditions, and for the form of…

physics.flu-dyn2025

Tradeoffs in Biconic Intake Aerodynamic Design Optimization with Sub-optimal Oswatitsch Solutions

J. P. S. Sandhu, M. Bhardwaj, N. Ananthkrishnan +3

The notion of sub-optimal Oswatitsch solutions is introduced in order to systematically conduct a tradeoff between total pressure recovery (TPR) and intake drag coefficient (CDi) f…

physics.flu-dyn2024

Zero-dimensional Analysis of Thermal Choking in Arbitrary Duct with Application to Dual-mode Ramjet Combustor

N Ananthkrishnan, K Sreesankar

Thermal choking in combustor ducts is a matter of great interest to researchers involved in the design and analysis of combustors. In case of scramjet combustors, a thermally choke…

physics.flu-dyn2024★ 1 cited

Turbojet Module Sizing for Integration with Turbine-Based Combined Cycle Engine

S. Rajashankar, N. Ananthkrishnan, A. Sharma +2

A turbine-based combined cycle (TBCC) vehicle is studied that relies on a scramjet engine for high-speed flight but requires a turbojet module to accelerate it to a high supersonic…

physics.flu-dyn2024★ 1 cited

Multi-Objective Aerodynamic Optimization of External Compression Supersonic Intake using Kriging/MOGA

JPS Sandhu, M Bhardwaj, N Ananthkrishnan +2

A formal optimization procedure is reported for an external-compression supersonic intake with the twin objectives of maximizing the total pressure recovery while simultaneously mi…