Results 11 to 20 of about 87,896 (266)

A Characterized Status Report on Pulse Detonation Engine [PDF]

open access: yesINCAS Bulletin, 2019
Pulse Detonation Engine (PDE), is an exciting propulsion technology for the future and has been able to seek considerable attention over the last era. It has the potential to work efficiently in the modern cosmos.
Bharat Ankur DOGRA   +2 more
doaj   +1 more source

Context Specificity in Stability of Hyperactivity–Impulsivity [PDF]

open access: yesEuropean Journal of Personality, 2010
This paper exemplifies a secondary data analysis of context–specific differences in children's hyperactivity–impulsivity while controlling for informant–specific effects. Participants were boys and girls from the NICHD Study of Early Child Care and Youth Development whose behaviours were measured in 1st, 3rd and 5th grades.
J, Kim   +3 more
openaire   +2 more sources

The energy potential of some high-enthalpy N-oxides as oxidizers [PDF]

open access: yesОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение", 2018
The energy abilities of solid composite propellants based on a couple of new high-enthalpy N-oxides (furazano-terazine-dioxide and tetrazino-tetrazine-1,3,6,8-tetraoxide) have been considered, it is found that these two compounds show record energy ...
D. B. Lempert   +2 more
doaj   +1 more source

Using the Impulse Method to Determine High-Pressure Dynamic Burning Rate of Solid Propellants

open access: yesAerospace, 2023
A new method for determining the burning rate of a solid propellant, called the Impulse Method, is proposed in this paper. It is based on the proportional relationship between the impulse generated and the mass of the burned propellant. The pressure–time
Jiahao Liu   +3 more
doaj   +1 more source

MODIFICATION OF THE ENERGY-SATURATED HETEROGENEOUS COMPOSITE MATERIAL BY CYCLIC NITRAMINES

open access: yesВесці Нацыянальнай акадэміі навук Беларусі: Серыя фізіка-тэхнічных навук, 2018
Several methods have been described for increasing the main characteristics (density, heat of combustion, combustion temperature, gas formation index) and operating properties (combustion speed and temperature, total and specific impulse, properties of ...
A. Ph. Ilyushchanka   +2 more
doaj   +1 more source

Pulsed Detonation Hydroramjet: Design Optimization

open access: yesJournal of Marine Science and Engineering, 2022
A new type of marine transportation engine, the pulsed detonation hydroramjet (PDH), which was first designed, manufactured, and tested by the present authors, has been further investigated in terms of the potential improvement of its propulsive ...
Sergey M. Frolov   +5 more
doaj   +1 more source

Effects of key parameters on performance of a pre-cooled core engine based on the closed helium cycle

open access: yesFrontiers in Mechanical Engineering, 2023
A pre-cooled combined engine based on a closed helium (He) cycle offers high specific thrust and high specific impulse. Therefore, evaluation of the performance of such an engine is crucial for engine applications and key technology research.
Ma Tong-Ling   +7 more
doaj   +1 more source

Control of Myelination by Specific Patterns of Neural Impulses [PDF]

open access: yesThe Journal of Neuroscience, 1998
A cell culture preparation equipped with stimulating electrodes was used to investigate whether action potential activity can influence myelination of mouse dorsal root ganglia axons by Schwann cells. Myelination was reduced to one-third of normal by low-frequency impulse activity (0.1 Hz), but higher-frequency stimulation (1 Hz) had no effect.
B, Stevens, S, Tanner, R D, Fields
openaire   +2 more sources

Modelling Rocket System Performance Parameters

open access: yesAcademy Journal of Science and Engineering, 2022
What distinguishes the rocket system from airbreathing engines is that the rocket carries its own propellants, fuel and oxidants.  The modern rocket was originally developed for ballistic missiles.
Nnorom Achara
doaj  

Liquid rocket engine performance assessment in the context of small launcher optimisation [PDF]

open access: yesINCAS Bulletin, 2019
The paper presents a fast mathematical model that can be used to quickly asses the propulsive characteristics of liquid propelled rocket engines. The main propulsive parameters are computed using combustion surfaces obtained after a nonlinear data ...
Alexandru-Iulian ONEL   +4 more
doaj   +1 more source

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