Download or read book tude th orique et exp rimentale de probl mes a rodynamiques concernant les compresseurs transsoniques written by Hubert Miton (auteur d'une thèse de sciences.) and published by . This book was released on 1978 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book tude th orique et exp rimentale de probl mes a rodynamiques concernant les compresseurs transsoniques written by Hubert Miton and published by . This book was released on 1978 with total page 454 pages. Available in PDF, EPUB and Kindle. Book excerpt: NATURE DES ECOULEMENTS DANS LES TURBOMACHINES. PRINCIPAUX MODELES. ETUDE DU DIFFUSEUR SUPERSONIQUE D'UN COMPRESSEUR CENTRIFUGE. APPLICATION DE LA METHODE DES ANALOGIES HYDRAULIQUES. VISUALISATION DES ECOULEMENTS PAR STRIOSCOPIE. ESSAI DE CONTROLE DU PHENOMENE D'INTERACTION ONDE DE CHOC-COUCHE LIMITE EN GRILLE D'AUBES. CALCUL D'ECOULEMENTS D'UN FLUIDE PARFAIT AVEC ONDES DE CHOC PAR UNE METHODE DE DIFFERENCES FINIES

Download or read book The Theory of Propellers written by Theodore Theodorsen and published by . This book was released on 1944 with total page 184 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: A technical method is given for calculating the axial interference velocity of a propeller. The method involves the use of certain weight functions P, Q, and F. Numerical values for the weight functions are given for two-blade, three-blade, and six-blade propellers.

Download or read book Transonic Aerodynamics written by L. Pamela Cook and published by SIAM. This book was released on 1993-01-01 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume offers exciting results, perspectives, and case studies for the treatment of problems arising in transonic aerodynamics. New advances including triple deck theory, analysis of stagnation at the nose of a body, transonic choked flow, and the transonic area rule are presented. Interest in analyzing the transonic range of flight, its stability properties, and especially the question of designing reduced drag (shockless or weak shock) airfoils keeps growing. Present day commercial aircraft cruise in the transonic range. Mechanical and aeronautical engineers interested in compressible fluid flows, design of optimal wings, and an understanding of transonic flow held about wings and airfoils will find the book invaluable. This book is understandable to those with a knowledge of continuum mechanics (fluids) and asymptotic methods. It is appropriate for graduate courses in aerodynamics and mathematical methods.