Author: Louis G. KaufmanPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 68
Book Description
Pressure and Thermal Distributions on Wings and Adjacent Surfaces Induced by Elevon Deflections at Mach 6
Author: Louis G. KaufmanPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 68
Book Description
NASA Technical Paper
Author: NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 824
Book Description
NASA Scientific and Technical Publications
Author: Pressure Distributions Induced by Elevon Deflections on Swept Wings and Adjacent End-plate Surfaces at Mach 6
Author: Louis G. Kaufman (II.)Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 132
Book Description
Turbulent Shear-Layer/Shock-Wave Interactions
Author: J. DeleryPublisher: Springer Science & Business Media
ISBN: 3642827705
Category : Science
Languages : en
Pages : 434
Book Description
It was on a proposal of the late Professor Maurice Roy, member of the French Academy of Sciences, that in 1982, the General Assembly of the International Union of Theoretical and Applied Mechanics decided to sponsor a symposium on Turbulent Shear-Layer/Shock-Wave Interactions. This sympo sium might be arranged in Paris -or in its immediate vicinity-during the year 1985. Upon request of Professor Robert Legendre, member of the French Academy of Sciences, the organization of the symposium might be provided by the Office National d'Etudes et de Recherches Aerospatiales (ONERA). The request was very favorably received by Monsieur l'Ingenieur General Andre Auriol, then General Director of ONERA. The subject of interactions between shock-waves and turbulent dissipative layers is of considerable importance for many practical devices and has a wide range of engineering applications. Such phenomena occur almost inevitably in any transonic or supersonic flow and the subject has given rise to an important research effort since the advent of high speed fluid mechanics, more than forty years ago. However, with the coming of age of modern computers and the development of new sophisticated measurement techniques, considerable progress has been made in the field over the past fifteen years. The aim of the symposium was to provide an updated status of the research effort devoted to shear layer/shock-wave interactions and to present the most significant results obtained recently.
Pressure and Thermal Distributions on Wings and Adjacent Surfaces Induced by Elevon Deflections at Mach 6
Author: Scientific and Technical Aerospace Reports
Author: Compendium of NASA Langley Reports on Hypersonic Aerodynamics
Author: Frances E. SaboPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 182
Book Description
Author: