Mach Five to Ten Morphing Waverider: Control Point Study-Reference-Cited by-同舟云学术

Mach Five to Ten Morphing Waverider: Control Point Study

Published:2019-03 Issue:2 Volume:56 Page:493-504
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Phoenix Austin A.¹,Rogers Robert E.¹,Maxwell Jesse R.¹,Goodwin Gabriel B.¹

Affiliation:

1. Naval Research Laboratory, Washington, D.C. 20375

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034901

Reference44 articles.

1. Hypersonic Waverider Stream Surface Actuation for Variable Design Point Operation

2. BowcuttK. G.AndersonJ. D.CapriottiD. “Numerical Optimization of Conical Flow Waveriders Including Detailed Viscous Effects,” Aerodynamics of Hypersonic Lifting Vehicles, AGARD CP-428, Neuilly-Sur-Seine, France, 1987.

3. Viscous optimized hypersonic waveriders designed from axisymmetric flow fields

4. Efficient Design of Viscous Waveriders with CFD Verification and Off-Design Performance Analysis

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