Download or read book Passive Control of Normal Shock boundary Layer Interaction Using Aeroelastic Mesoflaps written by Martin Johannes Orphanides and published by . This book was released on 2003 with total page 390 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experiments on Normal Shock boundary Layer Interaction Control Using Aeroelastic Mesoflaps written by Everett Shingo Hafenrichter and published by . This book was released on 2001 with total page 282 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Smart Mesoflaps for Aeroelastic Transpiration to Control Shock Boundary Layer Interactions written by and published by . This book was released on 2002 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The grant investigated a new concept in shock-wave/boundary-layer interaction control: tile use of aeroelastic mesoflaps to provide efficient recirculation transpiration. Appendix 1A presents a set of Power-Point slides which summarize the major finding of the study and also suggest a potential path forward to develop the technology and transition it to allow a bleedless supersonic inlet. As such, the goal would be to allow the overall benefits of a zero-bleed boundary layer control system into supersonic aircraft inlets: via retrofitting current inlets (e.g. the F-18E/F) or incorporating into design of future aircraft (e.g. the Long Range Strike Aircraft). As noted on Slide 2, the advantages of a bleedless inlet as evaluated by the aircraft industry are substantial and can considered in terms of either extended range (as much as 20%) or reduced gross take-off weight (as much as 10% as detailed in Part 7). As discussed on slides 2-9, tile aerodynamic benefits for tile mesoflaps over conventional recirculation transpiration with a porous plate include improved aerodynamics for subsonic conditions, more aerodynamic aerodynamic bleed and injection for shock interactions and increased shock stability. These benefits have been quantified for oblique impinging shocks, ramp-generated oblique shocks and normal shocks (Part 2). Additional research was conducted to understand tile structural dynamic issues (Parts 3 and 4) and how a closed-loop control system might be employed in order to allow further performance increases (Part 5). Appendix 1B gives an overview of the how these various research activities were integrated together.
Download or read book Simulations of Normal Shock Wave boundary Layer Interaction Control Using Mesoflaps written by Rajeev Kumar Jaiman and published by . This book was released on 2002 with total page 288 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Passive Control of Oblique Shock boundary Layer Interaction at High Mach Number written by V. Borovoy and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Study of Passive Control in a Transonic Shock Wave boundary Layer Interaction written by Reynald Bur and published by . This book was released on 1997 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book AIAA Journal written by American Institute of Aeronautics and Astronautics and published by . This book was released on 2002 with total page 1358 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book AIAA Aerospace Sciences Meeting and Exhibit 42nd written by and published by . This book was released on 2004 with total page 566 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics written by Kumar, Sathish K. and published by IGI Global. This book was released on 2022-06-24 with total page 429 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamics is a science that improves the ability to understand theoretical basics and apply fundamental physics in real-life problems. The study of the motion of air, both externally over an airplane wing and internally over a scramjet engine intake, has acknowledged the significance of studying both incompressible and compressible flow aerodynamics. The Handbook of Research on Aspects and Applications of Incompressible and Compressible Aerodynamics discusses all aspects of aerodynamics from application to theory. It further presents the equations and mathematical models used to describe and characterize flow fields as well as their thermodynamic aspects and applications. Covering topics such as airplane configurations, hypersonic vehicles, and the parametric effect of roughness, this premier reference source is an essential resource for engineers, scientists, students and educators of higher education, military experts, libraries, government officials, researchers, and academicians.
Download or read book 41st AIAA Aerospace Sciences Meeting Exhibit written by and published by . This book was released on 2003 with total page 684 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Aeronautical Journal written by and published by . This book was released on 2005 with total page 700 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book 40th AIAA Aerospace Sciences Meeting Exhibit written by and published by . This book was released on 2002 with total page 676 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book EUROSHOCK Drag Reduction by Passive Shock Control written by Egon Stanewsky and published by Springer Science & Business Media. This book was released on 2013-04-17 with total page 432 pages. Available in PDF, EPUB and Kindle. Book excerpt: This volume contains the description of an EC-sponsered program to study all relevant aspects of shock/ boundary-layer interaction control, the latter designed to improve aircraft performance at design (cruise) and off-design conditions. The work being presented includes a discussion of basic control experiments and the corresponding physical modeling, to account for shock control and a discussion of the airfoil experiments conducted for code validation and control assessment, in conjunction with the basic experiments and computations. The contents is comprised of a section giving a broad overview of the research carried out here and more detailed individual contributions by the participants in the research. Der Band enthält den Abschlußbericht eines von EU geförderten Projekts EUROSHOCK, das alle relevanten Aspekte der Kontrolle von Stoßfronten und Grenzschichten (wichtig z.B. für die Verbesserung der Flugeigenschaften von Fluzeugen) untersuchte. Neben einer ausführlichen Diskussion der grundlegenden Kontrollexperimente und der zugrundeliegenden Modellierung werden auch die Versuche an Tragflächen beschrieben, die zur Validierung von Modellrechnungen durchgeführt werden. Darüber hinaus enthält der Band auch die detaillierten Ergebnisse der Teilnehmer an dem Forschungsprogramm.
Download or read book 41st AIAA ASME SAE ASEE Joint Propulsion Conference Exhibit 10 13 July 2005 Tucson Arizona 05 4000 05 4049 written by and published by . This book was released on 2005 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Smart Mesoflaps for Control of Shock Boundary Layer Interactions written by E. Loth and published by . This book was released on 2000 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book 32nd AIAA Fluid Dynamics Conference and Exhibit written by and published by . This book was released on 2002 with total page 564 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Modeling and Control of a Smart Material Mesoflap System for Shock Boundary Layer Interaction Control written by Marina L. Tharayil and published by . This book was released on 2001 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt:
