In this work, startability of the Busemann intake family with weak/strong conical shock, as most efficient intakes, via overboard mass spillage method is theoretically analyzed. Masterix and Candifix codes are used to numerically simulate few models of this type of intake and verify the theoretical results. Portions of the intake corresponding to various flow capture angles are considered to have mass spillage in the starting process of this intake. This approach allows for overboard mass spillage via a V-shaped slot with the tip of V coinciding with the focal point of the Busemann flow. The theoretical results, achieved using two different theories, of self-started Busemann takes with weak/strong conical shock show that significant improve...
Hypersonic airbreathing propulsion is soon to become a viable means of transportation and hence dete...
To this date, there is no generally valid method to accurately predict intake starting for a certain...
The aerodynamic design of hypersonic inlets is a critical issue for the overall performance of an ai...
A review and summary is presented of hypersonic air intake technology highlighting design objectives...
Supersonic inlet starting by mass spillage is studied theoretically and numerically in the present t...
The classical approach to scramjet intake design, analysis, experimental testing, and performance as...
Designing high-performance air intakes is of crucial importance for the successful operation of hype...
AbstractThe impulse and self starting characteristics of a mixed-compression hypersonic inlet design...
This work investigates fluid mechanical processes involving movement of shock waves inside channels....
The purpose of this study was to create and investigate starting techniques aimed at allowing comple...
Starting of an intake is an essential aspect while considering the design of intake geometry (ref.1)...
The purpose of this study was to create and investigate starting techniques aimed at allowing comple...
Starting of an intake is an essential aspect while considering the design of intake geometry (ref.1)...
For efficient operation of an air-breathing hypersonic/supersonic engine its air intake must be star...
This report investigates the characteristic fluid mechanical phenomena occurring on a diverterless c...
Hypersonic airbreathing propulsion is soon to become a viable means of transportation and hence dete...
To this date, there is no generally valid method to accurately predict intake starting for a certain...
The aerodynamic design of hypersonic inlets is a critical issue for the overall performance of an ai...
A review and summary is presented of hypersonic air intake technology highlighting design objectives...
Supersonic inlet starting by mass spillage is studied theoretically and numerically in the present t...
The classical approach to scramjet intake design, analysis, experimental testing, and performance as...
Designing high-performance air intakes is of crucial importance for the successful operation of hype...
AbstractThe impulse and self starting characteristics of a mixed-compression hypersonic inlet design...
This work investigates fluid mechanical processes involving movement of shock waves inside channels....
The purpose of this study was to create and investigate starting techniques aimed at allowing comple...
Starting of an intake is an essential aspect while considering the design of intake geometry (ref.1)...
The purpose of this study was to create and investigate starting techniques aimed at allowing comple...
Starting of an intake is an essential aspect while considering the design of intake geometry (ref.1)...
For efficient operation of an air-breathing hypersonic/supersonic engine its air intake must be star...
This report investigates the characteristic fluid mechanical phenomena occurring on a diverterless c...
Hypersonic airbreathing propulsion is soon to become a viable means of transportation and hence dete...
To this date, there is no generally valid method to accurately predict intake starting for a certain...
The aerodynamic design of hypersonic inlets is a critical issue for the overall performance of an ai...