Add to ORKGA computer program for analyzing the nozzle for a hypersonic scramjet by a second order characteristic procedure is described. The program used FORTRAN IV. The input routine is provided. A sample input for a source flow case is included
The reference-plane method of characteristics is applied to the computation of the supersonic flow i...
The use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic ...
The progress report for the grant entitled 'Hypervelocity of Scramjet Combustor-Nozzle Analysis and ...
A FORTRAN IV program for analyzing the nozzle flow for a hypersonic scramjet by a two dimensional se...
The factors which influence the design and selection of a nozzle for a hypersonic scramjet are descr...
The FORTRAN IV Program developed to analyze the flow field associated with scramjet exhaust systems ...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
A second order numerical method employing reference plane characteristics has been developed for the...
A summary is presented of the various documents that discuss and describe the computer programs and ...
The process is discussed of designing a nozzle for a hypersonic airbreathing vehicle which involves ...
FORTRAN 4 program for computerized design of two dimensional supersonic nozzles with sharp edged thr...
A computer program was developed to describe the performance of ramjet and scramjet cycles. The prog...
A computer program for analyzing two dimensional and axisymmetric nozzle performance with a variety ...
A computer program previously developed to analyze three-dimensional supersonic nozzles by the metho...
This report summarizes work accomplished under Contract No. NAS1-12726 towards the development of co...
The reference-plane method of characteristics is applied to the computation of the supersonic flow i...
The use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic ...
The progress report for the grant entitled 'Hypervelocity of Scramjet Combustor-Nozzle Analysis and ...
A FORTRAN IV program for analyzing the nozzle flow for a hypersonic scramjet by a two dimensional se...
The factors which influence the design and selection of a nozzle for a hypersonic scramjet are descr...
The FORTRAN IV Program developed to analyze the flow field associated with scramjet exhaust systems ...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
A second order numerical method employing reference plane characteristics has been developed for the...
A summary is presented of the various documents that discuss and describe the computer programs and ...
The process is discussed of designing a nozzle for a hypersonic airbreathing vehicle which involves ...
FORTRAN 4 program for computerized design of two dimensional supersonic nozzles with sharp edged thr...
A computer program was developed to describe the performance of ramjet and scramjet cycles. The prog...
A computer program for analyzing two dimensional and axisymmetric nozzle performance with a variety ...
A computer program previously developed to analyze three-dimensional supersonic nozzles by the metho...
This report summarizes work accomplished under Contract No. NAS1-12726 towards the development of co...
The reference-plane method of characteristics is applied to the computation of the supersonic flow i...
The use of a computer code for the calculation of two dimensional inlet flow fields in a supersonic ...
The progress report for the grant entitled 'Hypervelocity of Scramjet Combustor-Nozzle Analysis and ...