Results 101 to 110 of about 2,233 (228)

Boru bağlantılı ramjet test düzeneğinin nümerik ve deneysel incelenmesi. [PDF]

open access: yes, 2014
The main objective of this study is to make a numerical model of direct connected ramjet test facility which is used for ground tests of supersonic air breathing propulsion systems.
Esirgen, Başar
core  

Multi-Channel Gliding Arc Plasma Cracking of RP-3 Kerosene Spray

open access: yesEnergies
To address the issues of narrow ignition limits and low combustion efficiency in ramjet combustors under low-temperature and low-pressure conditions, caused by low reactivity of liquid fuel and slow chemical reaction rates, a multi-channel gliding arc ...
Shengfang Huang   +4 more
doaj   +1 more source

Zero-Dimensional Ignition Model of Boron Agglomerates. [PDF]

open access: yesACS Omega, 2023
Duan L   +6 more
europepmc   +1 more source

Numerical Investigation of Scaling Effects of a Ramjet-Powered Projectile [PDF]

open access: yes, 2019
Ramjet flowpath miniaturization is a potentially useful technology for integration into munitions to increase range, accuracy, and lethality. The emphasis of this effort is to numerically characterize the performance of a miniature hydrogen-fueled and ...
Vedam, Arjun Jaishankar
core   +1 more source

H2 fueled flightweight ramjet construction and test [PDF]

open access: yes, 1992
The ACES Program began the investigation of regeneratively cooled ramjet engines for propelling aircraft at Mach 6 to 8 flight regimes while collecting and processing air for later use as oxidizer in rocket propulsion into an orbit flight mode.
Malek, Albert
core   +1 more source

Missile Industry-Marquardt-Ramjet Engine P.1 [PDF]

open access: yes
Marquardt Corporation RJ43-MA-11 Ramjet Engine.

core  

H∞ Robust Control of Ramjet Engine [PDF]

open access: yes, 2020
Ramjet engine presents the simplest type of jet engines since it does not possess moving parts, like compressors, shafts and turbines. Besides its simplicity, it provides efficient performances in a wide range of altitudes, supersonic speeds and angles
Zorić, Nemanja   +3 more
core  

Endothermic fuels for supersonic ramjet

open access: yes, 2003
Fluid Mechanics & Internal Ballistics Division, Propulsion Group, Vikram Sarabhai Space Centre, Trivandrum-695 022, India E-mail : ddeepak@vsnl.net Fax: 91-471-562060 Manuscript received 17 December 2002 Greater ease of use and higher density make hydrocarbon fuels an attractive option for hypersonic space transport vehicle.
Desh Deepak, R. Jeenu
openaire   +2 more sources

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