Evolution of Supersonic Modes in Hypersonic High-Enthalpy Boundary Layer Transition
With continuous expansion of flight speed and altitude domains, the high-temperature gas effects, especially the thermochemical non-equilibrium (TCNE) effects in hypersonic high-enthalpy boundary layers invalidated the calorically perfect gas (CPG ...
Zhou-yuan ZHAO +3 more
doaj +1 more source
Direct Images of the Virtual Source in a Supersonic Expansion
Direct images of the virtual source in a supersonic expansion of helium are presented. The images were obtained using a Fresnel zone plate with free-standing zones, 540 microm in diameter and with an outermost zone width of 50 nm. The general method can be extended to other beams, including seeded beams. Measurements were carried out at absolute source
REISINGER T +5 more
openaire +6 more sources
PENETRATION OF A SHOCK WAVE IN A FLAME FRONT [PDF]
The present paper deals with the interactions between a fully supersonic flame front, situated in a supersonic two-dimensional flow of an ideal homogeneous combustible gas mixture, and an incident shock wawe, which is penetrating in the space of the hot ...
Dan PANTAZOPOL
doaj +1 more source
Supersonic Diversions: Assessment of Great-Circle versus Sonic Boom-Restricted Flight Routing [PDF]
Overland supersonic flight bans due to the sonic boom are often said to be the reason for civil high-speed aircraft not being able to make a breakthrough.
Bernd Liebhardt +5 more
core +1 more source
Properties of water and argon clusters developed in supersonic expansions
Using adiabatic molecular dynamics coupled with the fluid dynamics equations, we model nucleation in an expanding beam of water vapor and argon on a microsecond scale. The size distribution of clusters, their temperature, and pickup cross sections in dependence on velocity are investigated and compared to the geometric cross sections and the experiment.
Martin Klíma +3 more
openaire +3 more sources
Theoretical Study of a Novel CO2 Supersonic Two-phase Expansion Refrigeration Cycle
Natural refrigerants such as CO2 have become a research hotspot. Under high-pressure conditions, a large throttling loss becomes the primary reason for the low circulation efficiency of the CO2 refrigeration cycle. Therefore, reducing the throttling loss
Zeng Yupei +6 more
doaj
Expansion Waves at the Outlet of the Supersonic Two-Phase Flow Nozzle
Two-phase flow nozzles are used in the total flow system of geothermal power plants and in the ejector of the refrigeration cycle, etc. One of the most important functions of the two-phase flow nozzle is converting two-phase flow thermal energy into ...
Masafumi NAKAGAWA +3 more
doaj +1 more source
Estimation of the Market Potential for Supersonic Airliners via Analysis of the Global Premium Ticket Market [PDF]
This study assesses the global market potential for supersonic airline transportation by evaluating worldwide premium ticket sales figures based on so-called marketing information data tapes (MIDTs).
Bernd Liebhardt +5 more
core +1 more source
Aerodynamic Control and Mixing with Ramp Injection [PDF]
Experiments have been conducted in the GALCIT Supersonic Shear Layer Facility (S3L) to investigate the behaviour of a flow and geometry with many features that are potentially useful for a Supersonic Combustion Ramjet (SCRAMJET) engine - a recirculation ...
Johnson, Michael Bernard
core +1 more source
Mixing Characteristics of Supersonic Jets Injected into a Pressurized Gas Environment
The transition toward carbon-neutral energy systems has accelerated interest in hydrogen-fueled combustion technologies, where efficient fuel–air mixing is essential for stable and clean combustion.
Miah Md Ashraful Alam +5 more
doaj +1 more source

