Author: Richard D. SamuelsPublisher:
ISBN:
Category : Skim friction (Aerodynamics)
Languages : en
Pages : 82
Book Description
Experimental Investigation of the Turbulent Boundary Layer at a Mach Number of 6 with Heat Transfer at High Reynolds Numbers
Author: Richard D. SamuelsPublisher:
ISBN:
Category : Skim friction (Aerodynamics)
Languages : en
Pages : 82
Book Description
Experimental Investigation of a Turbulent Boundary Layer at Mach 6, High Reynolds Numbers, and Zero Heat Transfer
Author: Jerry B. AdcockPublisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 66
Book Description
NASA Technical Note
Author: Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory
Author: Michael C. FischerPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 66
Book Description
Wind tunnel investigation of laminar, transitional, and turbulent boundary layer profiles on wedge at hypersonic speed to confirm theoretical analysis.
NASA Technical Paper
Author: Applied Mechanics Reviews
Author: Government-wide Index to Federal Research & Development Reports
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1794
Book Description
Shock Wave-Boundary-Layer Interactions
Author: Holger BabinskyPublisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481
Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.
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