An Euler Numerical Study of Busemann and Quasi-Busemann Hypersonic Inlets at On- and Off-Design Speeds
Author:
Affiliation:
1. University of Maryland
2. University of Colorado
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-66
Reference16 articles.
1. The Impact of Round Combustors on TBCC Propulsion and Hypersonic Cruise Vehicles
2. High Aspect Ratio Isolator Performance for Access-to-Space Vehicles
3. Design and analysis of streamline traced hypersonic inlets
4. Hypersonic Inward Turning Inlets: Design and Optimization
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1. Control-Volume-Based Exergy Method of Truncated Busemann Inlets in Off-Design Conditions;Processes;2024-03-07
2. Numerical Evaluation of Hypersonic Inward-Turning Inlets at Off-Design Mach Number;AIAA SCITECH 2023 Forum;2023-01-19
3. Optimal aerodynamic design of hypersonic inlets by using streamline-tracing techniques;ADV AIRCR SPACECR SC;2020
4. A new integration method based on the coupling of mutistage osculating cones waverider and Busemann inlet for hypersonic airbreathing vehicles;Acta Astronautica;2016-09
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