Add to ORKGThis report presents the results of the computational work carried out for the lift analysis of LCA wings in supersonic flows using a computer software called LAWS [1]. The lifting pressure distribution and the associated force coefficients\ud have been obtained for three planforms specified by the LCA group
An integrated system of computer programs was developed for the design and analysis of supersonic co...
The method of relating the solution of a flow field to the solution of a simpler or known boundary-v...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
A computer program 'called LAWS has been developed for the Lift Analysis of Wings In Supersonic flow...
A computer program 'called LAWS has been developed for the Lift Analysis of Wings In Supersonic flow...
Euler calculations are necessary for the prediction of vortex dominated flows encountered by modern ...
Euler calculations are necessary for the prediction of vortex dominated flows encountered by modern ...
Loading Is An Important Phase Of The Structural Analysis And Design Cycle . In This Phase, Various L...
A general purpose computer code called ' PHOENICS' has been used to compute flow field in an air in...
Loading Is An Important Phase Of The Structural Analysis And Design Cycle . In This Phase, Various L...
A new method has been developed for calculating the pressure distribution and aerodynamic characteri...
A description of and users manual are presented for a U.S.A. FORTRAN 4 computer program which evalua...
A general purpose computer code called ' PHOENICS' has been\ud used to compute flow field in an air ...
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back w...
Supplementary information for computer program predicting lifting pressure and camber shape of compo...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
The method of relating the solution of a flow field to the solution of a simpler or known boundary-v...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
A computer program 'called LAWS has been developed for the Lift Analysis of Wings In Supersonic flow...
A computer program 'called LAWS has been developed for the Lift Analysis of Wings In Supersonic flow...
Euler calculations are necessary for the prediction of vortex dominated flows encountered by modern ...
Euler calculations are necessary for the prediction of vortex dominated flows encountered by modern ...
Loading Is An Important Phase Of The Structural Analysis And Design Cycle . In This Phase, Various L...
A general purpose computer code called ' PHOENICS' has been used to compute flow field in an air in...
Loading Is An Important Phase Of The Structural Analysis And Design Cycle . In This Phase, Various L...
A new method has been developed for calculating the pressure distribution and aerodynamic characteri...
A description of and users manual are presented for a U.S.A. FORTRAN 4 computer program which evalua...
A general purpose computer code called ' PHOENICS' has been\ud used to compute flow field in an air ...
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back w...
Supplementary information for computer program predicting lifting pressure and camber shape of compo...
An integrated system of computer programs was developed for the design and analysis of supersonic co...
The method of relating the solution of a flow field to the solution of a simpler or known boundary-v...
An integrated system of computer programs was developed for the design and analysis of supersonic co...