Aerodynamic Measurements of an Air-Breathing Hypersonic Vehicle at Mach 3.5 to 8-Reference-Cited by-同舟云学术

Aerodynamic Measurements of an Air-Breathing Hypersonic Vehicle at Mach 3.5 to 8

Published:2018-11 Issue:11 Volume:56 Page:4282-4296
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Gruhn Patrick¹,Gülhan Ali¹

Affiliation:

1. DLR, German Aerospace Center, 51147 Cologne, Germany

Funder

FP7 Transport

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J056522

Reference26 articles.

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3. An Aerodynamic Analysis of Several Hypersonic Research Airplane Concepts from M= 0.2 to 6.0

4. Aerodynamic and Inlet Flow Characteristics of Several Hypersonic Airbreathing Missile Concepts

5. Hypersonic aircraft optimization including aerodynamic, propulsion, and trim effects

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