A hypersonic rarefied diatomic gas flow around a delta wing with a blunted leading edge at an angle of attack of 10° is considered. Flow fields on the leeward and windward sides are obtained. Specific features of surface distributions of thermal characteristics on the side edge are studied
The main objective of this project is to investigate the flow characteristics of the VFE- 2 blunt ed...
Delta wings have found wide application in a variety of aerospace vehicles including high performanc...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
A hypersonic rarefied diatomic gas flow around a delta wing with a blunted leading edge at an angle ...
To understand Mach number effect on flow field over a delta wing with blunt leading edge in superson...
The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds ...
The developments of highly maneuverable aircraft have prompted the extensive studies of the flow pas...
The investigation of a supersonic flow around a wing at the high angle of attack is of prac-tical in...
Euler and Navier-Stokes results are presented for a blunt delta wing at Mach 7.15 and 300 angle of ...
A survey was made of the parameters affecting the development of the leeward symmetric separated flo...
Delta wings have found wide application in a variety of aerospace vehicles including high performanc...
An experimental investigation of the lee-side flow on sharp leading-edge delta wings at supersonic s...
Available experimental data on a 65xB0; swept back cropped delta wing with rounded leading edges hav...
Delta wings have found wide application in a variety of aerospace vehicles including high performanc...
The features of the different types of flow on the lee surface of delta wings at supersonic speeds h...
The main objective of this project is to investigate the flow characteristics of the VFE- 2 blunt ed...
Delta wings have found wide application in a variety of aerospace vehicles including high performanc...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
A hypersonic rarefied diatomic gas flow around a delta wing with a blunted leading edge at an angle ...
To understand Mach number effect on flow field over a delta wing with blunt leading edge in superson...
The flow of a perfect gas over the slab portion of a blunted delta wing flying at hypersonic speeds ...
The developments of highly maneuverable aircraft have prompted the extensive studies of the flow pas...
The investigation of a supersonic flow around a wing at the high angle of attack is of prac-tical in...
Euler and Navier-Stokes results are presented for a blunt delta wing at Mach 7.15 and 300 angle of ...
A survey was made of the parameters affecting the development of the leeward symmetric separated flo...
Delta wings have found wide application in a variety of aerospace vehicles including high performanc...
An experimental investigation of the lee-side flow on sharp leading-edge delta wings at supersonic s...
Available experimental data on a 65xB0; swept back cropped delta wing with rounded leading edges hav...
Delta wings have found wide application in a variety of aerospace vehicles including high performanc...
The features of the different types of flow on the lee surface of delta wings at supersonic speeds h...
The main objective of this project is to investigate the flow characteristics of the VFE- 2 blunt ed...
Delta wings have found wide application in a variety of aerospace vehicles including high performanc...
When a thin delta wing with high leading-edge sweep is placed at incidence in a stream, the fluid se...
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