Accession Number : ADA186719


Title :   New Techniques in Computational Aerodynamics.


Descriptive Note : Final rept. 1 Jun 83-28 Feb 87,


Corporate Author : BROWN UNIV PROVIDENCE RI DIV OF APPLIED MATHEMATICS


Personal Author(s) : Sirovich, Lawrence


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a186719.pdf


Report Date : 06 Aug 1987


Pagination or Media Count : 95


Abstract : A wide range of problems in gas dynamics have been considered. Advances in subsonic, transonic, and supersonic gasdynamics have been made. The emphasis has been made on computational procedures both numerical and algebraic. This work has a strong basis in analytical methods, and goal has been to produce computational efficient codes which made optimal use of analytically known results. Keywords: Airfoils; Compressible flow; Pressure distribution; Supersonic; Inviscid flow; Three dimensional flow; Supersonic axisymmetric flow.


Descriptors :   *SUPERSONIC CHARACTERISTICS , *SUBSONIC CHARACTERISTICS , *TRANSONIC CHARACTERISTICS , *NUMERICAL METHODS AND PROCEDURES , AIRFOILS , COMPUTATIONS , COMPUTATIONS , OPTIMIZATION , AXISYMMETRIC FLOW , SUPERSONIC FLOW , THREE DIMENSIONAL FLOW , COMPRESSIBLE FLOW , CODING , EFFICIENCY , GAS DYNAMICS , PRESSURE DISTRIBUTION , RANGE(EXTREMES) , INVISCID FLOW


Subject Categories : Fluid Mechanics


Distribution Statement : APPROVED FOR PUBLIC RELEASE