LAPCAT II : conceptual design of a Mach 8 TBCC civil aircraft, enforced by full Navier-Stokes 3D nose-to-tail computation-Reference-Cited by-同舟云学术

LAPCAT II : conceptual design of a Mach 8 TBCC civil aircraft, enforced by full Navier-Stokes 3D nose-to-tail computation

Published:2011-04-11 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Defoort Sebastien¹,Ferrier Marc¹,Serre Laurent¹,Pastre Jean-Louis¹,Paridaens Christophe²,Scherrer Dominique¹,Ingenito Antonella³,Hendrick Patrick²,Bruno Claudio³

Affiliation:

1. ONERA

2. Université Libre de Bruxelles

3. University of Rome "La Sapienza"

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2317

Reference10 articles.

1. 3A.IngenitoandC.Bruno,"SizingofHypersonicAirbreathingVehicles",AIAA2009-5186,45thJointPropulsionConference &Exhibit,Denver,Colorado,USA,August2009.

2. Integrated Aeropropulsive Computational Fluid Dynamics Methodology for the Hyper-X Flight Experiment

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Analysis of factors determining numerical solution in the calculation of flow with combustion using the ONERA experimental model;Thermophysics and Aeromechanics;2023-10-23

2. An Improved Method for Initial Sizing of Airbreathing Hypersonic Aircraft;Aerospace;2023-02-18

3. Analysis of energy cascade utilization in the chemically precooled engine cycle from a perspective of indirect combustion;Fuel;2023-02

4. Propulsion Cycles;Airbreathing Hypersonic Propulsion;2023

5. Thermodynamic analysis for a novel steam Rankine cycle based indirect chemical precooled engine used for supersonic flight;Fuel;2022-08