CFD and experimental study of an inflatable re-entry vehicle model at Mach 3 conditions-Reference-Cited by-同舟云学术

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CFD and experimental study of an inflatable re-entry vehicle model at Mach 3 conditions

Published:2007-11 Issue:10 Volume:61 Page:854-865
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Terry Jai,Barber Tracie

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference13 articles.

1. M. Kruijff, E.J van der Heide, YES2, the second Young Engineers’ Satellite, A Tethered Inherently Safe Capsule, IAC-02-P.P.01, 2002.

2. SPRInT Technical Design Report, Delft University of Technology, 2000.

3. Hypersonic Aerothermodynamics;Bertin,1994

4. Hypersonic and High Temperature Gas Dynamics;Anderson,1989

5. Fluid-Dynamic Drag: Practical Information on Aerodynamic Drag and Hydrodynamic Resistance;Hoerner,1958

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1. Computational Analysis of Re-entry Space Vehicle at Supersonic and Hypersonic Speed;Solutions for Maintenance Repair and Overhaul;2023-11-09

2. Numerical Simulation of Base Pressure and Drag of Space Reentry Capsules at High Speed;Hypersonic Vehicles - Past, Present and Future Developments;2019-10-02

3. Transient analysis of counterflowing jet over highly blunt cone in hypersonic flow;Acta Astronautica;2012-04

4. High speed flow characteristics in gun tunnel;AIP Conference Proceedings;2012

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