Add to ORKGAlso known as Aero-Rept--9217SIGLEAvailable from British Library Document Supply Centre- DSC:6015.42F(N--96-12382)(microfiche) / BLDSC - British Library Document Supply CentreGBUnited Kingdo
This paper examines the Shock/Shock Interactions (SSI) between the body and wing of aircraft in supe...
A Scramjet propulsion system is a form of airbreating jet engine using the high velocity of the air ...
Of all the possible outcomes of the shock interaction problem, Edney Type-III and Type-IV are consid...
The problem of three-dimensional steady shock wave interaction is a key issue for supersonic and hyp...
The problem of shock-shock interaction between a planar oblique shock wave and a bow shock wave is u...
SIGLEAvailable from British Library Document Supply Centre-DSC:D063067 / BLDSC - British Library Doc...
SIGLEAvailable from British Library Document Supply Centre- DSC:D79662 / BLDSC - British Library Doc...
The interactions of oblique/bow shock waves are the key flow phenomena restricting the design and ae...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX89586 / BLDSC - British Library Do...
The vast majority of shock wave–boundary-layer interactions in practical applications like supersoni...
Fiche copy of Aeronautical Internal Report no. 9112Available from British Library Document Supply Ce...
SIGLEAvailable from British Library Document Supply Centre- DSC:9113.125(UMIST-TFD--91/5) / BLDSC - ...
The shock-shock interaction in front of a cylinders is investigated numerically to identify the peak...
A kinetic, particle method has been used to model laminar shock-shock interactions of hypersonic flo...
Communication to : 3rd international symposium on atmospheric reentry vehicles and systems, Arcachon...
This paper examines the Shock/Shock Interactions (SSI) between the body and wing of aircraft in supe...
A Scramjet propulsion system is a form of airbreating jet engine using the high velocity of the air ...
Of all the possible outcomes of the shock interaction problem, Edney Type-III and Type-IV are consid...
The problem of three-dimensional steady shock wave interaction is a key issue for supersonic and hyp...
The problem of shock-shock interaction between a planar oblique shock wave and a bow shock wave is u...
SIGLEAvailable from British Library Document Supply Centre-DSC:D063067 / BLDSC - British Library Doc...
SIGLEAvailable from British Library Document Supply Centre- DSC:D79662 / BLDSC - British Library Doc...
The interactions of oblique/bow shock waves are the key flow phenomena restricting the design and ae...
SIGLEAvailable from British Library Document Supply Centre- DSC:DX89586 / BLDSC - British Library Do...
The vast majority of shock wave–boundary-layer interactions in practical applications like supersoni...
Fiche copy of Aeronautical Internal Report no. 9112Available from British Library Document Supply Ce...
SIGLEAvailable from British Library Document Supply Centre- DSC:9113.125(UMIST-TFD--91/5) / BLDSC - ...
The shock-shock interaction in front of a cylinders is investigated numerically to identify the peak...
A kinetic, particle method has been used to model laminar shock-shock interactions of hypersonic flo...
Communication to : 3rd international symposium on atmospheric reentry vehicles and systems, Arcachon...
This paper examines the Shock/Shock Interactions (SSI) between the body and wing of aircraft in supe...
A Scramjet propulsion system is a form of airbreating jet engine using the high velocity of the air ...
Of all the possible outcomes of the shock interaction problem, Edney Type-III and Type-IV are consid...