Research On Aeroelastic Phenomena In Airfoil Cascades An Experimental Investigation Of The Unsteady Aerodynamics Of A Classical Airfoil Cascade In Translation
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Aircraft Propulsion Systems Technology And Design
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Author : Gordon C. Oates
language : en
Publisher: AIAA
Release Date : 1989
Aircraft Propulsion Systems Technology And Design written by Gordon C. Oates and has been published by AIAA this book supported file pdf, txt, epub, kindle and other format this book has been release on 1989 with Aircraft gas-turbines categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1978
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Aeronautics categories.
Nasa Sp
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Author :
language : en
Publisher:
Release Date : 1979
Nasa Sp written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aeronautics categories.
Research On Aeroelastic Phenomena In Airfoil Cascades An Experimental Investigation Of The Unsteady Aerodynamics Of A Classical Airfoil Cascade In Translation
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Author : Sanford Fleeter
language : en
Publisher:
Release Date : 1978
Research On Aeroelastic Phenomena In Airfoil Cascades An Experimental Investigation Of The Unsteady Aerodynamics Of A Classical Airfoil Cascade In Translation written by Sanford Fleeter and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with categories.
The advent of high tip-speed, high work, blading in the fan stages of advanced gas turbine engines has led to the recognition of a new type of blading instability - unstalled supersonic flutter. As a result, a concerted effort to develop an appropriate predictive mathematical model has taken place. To determine the range of validity and to direct refinements to the basic flow model, fundamental supersonic oscillating cascade data are required. The experiment described herein is directed at significantly extending the range of existing supersonic cascade data to include translation mode oscillations. In particular, the fundamental time-variant translation mode aerodynamics are determined for the first time for a classical airfoil cascade in supersonic inlet flow field over a range of interblade phase angles at a realistic reduced frequency value. These unique experimental data are then correlated with predictions obtained from an appropriate state-of-the-art harmonically oscillating flat plate cascade aerodynamic analysis. (Author).
Aeronautical Engineering
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Author :
language : en
Publisher:
Release Date : 1979
Aeronautical Engineering written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1979 with Aeronautics categories.
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Government Reports Annual Index
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Author :
language : en
Publisher:
Release Date : 1978
Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978 with Government reports announcements & index categories.
Government Reports Announcements Index
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Author :
language : en
Publisher:
Release Date : 1978-06
Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1978-06 with Science categories.
Research On Aeroelastic Phenomena In Airfoil Cascades An Experimental Investigation Of The Unsteady Aerodynamics Of A Controlled Oscillating Mca Airfoil Cascade
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Author : Sanford Fleeter
language : en
Publisher:
Release Date : 1976
Research On Aeroelastic Phenomena In Airfoil Cascades An Experimental Investigation Of The Unsteady Aerodynamics Of A Controlled Oscillating Mca Airfoil Cascade written by Sanford Fleeter and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with categories.
A unique unsteady cascade experiment directed at providing fundamental aerodynamic data needed to verify or direct refinements to the basic model on unstalled supersonic torsional flutter in turbomachines is presented. In particular, the steady, quasi-static, and unsteady aerodynamics were determined for a multiple circular arc (MCA) airfoil cascade which modeled the tip section of an advanced design fan blade. The MCA cascade was harmonically oscillated in the torsional mode at a reduced frequency value of 0.14. The fundamental unsteady aerodynamic data was obtained at a Mach number equal to 1.55 over a range of interblade phase angles for two values of the cascade static pressure ratio. These unsteady results were then correlated with the predictions from state-of-the-art unsteady flat plate cascade analyses.
87 2050 87 2099
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Author :
language : en
Publisher:
Release Date : 1987
87 2050 87 2099 written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1987 with Airplanes categories.
International Aerospace Abstracts
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Author :
language : en
Publisher:
Release Date : 1995
International Aerospace Abstracts written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.