Results 201 to 210 of about 6,709 (233)

SURVEY OF NATIONAL RAMJET PROGRAM

1950
Abstract : The ramjet engine program has 8 groups engaged in development and testing projects covering engines designed for M = 2.0 to 4.0 and ranging in diameter from 14 to 43 in. Of these, two 20-in. engines are being developed solely for research purposes; the others are applicable to specific guided missiles (the Navajo (Mk770), Talos, Meteor ...
openaire   +1 more source

Effects of cavity length on operating characteristics of a ramjet rotating detonation engine fueled by liquid kerosene

Fuel, 2023
Wenkang Feng, Quan Zheng, Qiang Xiao
exaly  

Experimental investigation on the thrust regulation of a Mg–CO2 Martian ramjet

Acta Astronautica, 2022
Xu Wang
exaly  

Aerodynamic principles of shock-induced combustion ramjet engines

Aerospace Science and Technology, 2020
Zijian Zhang, Yunfeng Liu, Zonglin Jiang   +2 more
exaly  

Effects of new solid propellant configurations on the combustion characteristics of a ramjet

Aerospace Science and Technology, 2021
Ömer Musa, Guoping Huang, Zonghan Yu
exaly  

Wind tunnel tests of a hydrogen-fueled detonation ramjet model at approach air stream Mach numbers from 4 to 8

International Journal of Hydrogen Energy, 2017
S M Frolov, V S Ivanov, I O Shamshin
exaly  

Thermodynamic performance analysis of ramjet engine at wide working conditions

Acta Astronautica, 2017
Wei Huang
exaly  

Using exergy for performance evaluation of a conceptual ramjet engine burning hydrogen fuel

International Journal of Hydrogen Energy, 2018
Yasin Şöhret, Selcuk Ekici, T Hikmet Karakoc   +2 more
exaly  

The control optimization of low-orbit spacecraft with electric ramjet

Acta Astronautica, 2019
Alexander S Filatyev, Olga Yanova
exaly  

Comparison between ejector-ramjets and turbo-ramjets for T.S.T.O. propulsion

5th International Aerospace Planes and Hypersonics Technologies Conference, 1993
openaire   +1 more source