Status and trends in development of hypersonic integration configuration with dorsal intake

S Luo, Y Sun, J Liu, J Song - Aerospace Science and Technology, 2023 - Elsevier
The novel dorsal intake hypersonic configuration has become a research hotspot in the
aerospace industry due to its superior aerodynamic and inlet performance at small angles of …

Conceptual design of the high-speed propelled experimental flight test vehicle HEXAFLY

J Steelant, T Langener, K Hannemann… - 20th AIAA international …, 2015 - arc.aiaa.org
A concise overview of the overall layout of an experimental powered high-speed flight
vehicle including its subsystems is given. A mission scenario, the different flight segments …

Performance analysis of the hypersonic vehicle with dorsal and ventral intake

S Luo, Y Sun, J Liu, J Song, W Cao - Aerospace Science and Technology, 2022 - Elsevier
The integrated design of the airframe and inlet is the favorite choice for the aerodynamic
configuration design of the air-breathing hypersonic vehicle. To better understand the …

Optimization of scramjet inlet based on temperature and Mach number of supersonic combustion

PPB Araújo, MVS Pereira, GS Marinho… - Aerospace science and …, 2021 - Elsevier
A two-dimensional mixed compression scramjet inlet design is presented in this work. The
design is based on the static temperature and Mach number at the combustion chamber …

An aerothermodynamic design optimization framework for hypersonic vehicles

S Di Giorgio, D Quagliarella, G Pezzella… - Aerospace Science and …, 2019 - Elsevier
In the aviation field great interest is growing in passengers transportation at hypersonic
speed. This requires, however, careful study of the enabling technologies necessary for the …

CFD design capabilities for next generation high-speed aircraft

A Viviani, A Aprovitola, G Pezzella, C Rainone - Acta Astronautica, 2021 - Elsevier
Current design requirements are shaping advanced and efficient supersonic or hypersonic
aircraft concepts, capable of flying between distant parts of the globe within hours, and …

Low speed lateral-directional aerodynamic and static stability analysis of a hypersonic waverider

T Bykerk, D Verstraete, J Steelant - Aerospace Science and Technology, 2020 - Elsevier
Hypersonic waveriders have the potential to significantly reduce travel times on long haul
civilian transport routes. The design of hypersonic aircraft is heavily influenced by the …

Basic static stability and control characteristics of hypersonic vehicles with dorsal and ventral intake

S Luo, Y Sun, J Liu, J Song, W Cao - Aerospace Science and Technology, 2023 - Elsevier
The airframe/engine integrated configurations with dorsal intake can effectively decouple the
inlet from the lifting surface, leading to an excellent aerodynamic performance at a small …

Heat addition with variable area: Methodology for preliminary design of the scramjet combustion chamber

R Carneiro, A Passaro, PGP Toro - Physics of Fluids, 2023 - pubs.aip.org
Well-known analytical approaches are commonly adopted for the preliminary design of
scramjet engines. In this context, the combustion process in the combustion chamber can be …

[PDF][PDF] Aerodynamic design analysis of the HEXAFLY-INT hypersonic glider

G Pezzella, M Marini, B Reimann… - 20th AIAA International …, 2015 - researchgate.net
I. Introduction ver the last years, innovative concepts of civil high-speed transportation
vehicles were propose d 1, 2. These vehicles have a strong potential to increase the cruise …