Flow Visualization Studies of VTOL Aircraft Models During Hover in Ground Effect

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ISBN 13 :
Total Pages : 80 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Flow Visualization Studies of VTOL Aircraft Models During Hover in Ground Effect by :

Download or read book Flow Visualization Studies of VTOL Aircraft Models During Hover in Ground Effect written by and published by . This book was released on 1995 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow Visualization Studies of VTOL Aircraft Models During Hover in Ground Effect, Nikos J. Mourtos Et Al NASA, Ames Research Center, January 1995

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ISBN 13 :
Total Pages : pages
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Book Synopsis Flow Visualization Studies of VTOL Aircraft Models During Hover in Ground Effect, Nikos J. Mourtos Et Al NASA, Ames Research Center, January 1995 by :

Download or read book Flow Visualization Studies of VTOL Aircraft Models During Hover in Ground Effect, Nikos J. Mourtos Et Al NASA, Ames Research Center, January 1995 written by and published by . This book was released on with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)

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Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalogue, United States Public Documents

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ISBN 13 :
Total Pages : 856 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Monthly Catalogue, United States Public Documents by :

Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1995-10 with total page 856 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Slipstream Flow Around Several Tilt-wing VTOL Aircraft Models Operating Near the Ground

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ISBN 13 :
Total Pages : 76 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Slipstream Flow Around Several Tilt-wing VTOL Aircraft Models Operating Near the Ground by : William A. Newsom

Download or read book Slipstream Flow Around Several Tilt-wing VTOL Aircraft Models Operating Near the Ground written by William A. Newsom and published by . This book was released on 1962 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Monthly Catalog of United States Government Publications

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ISBN 13 :
Total Pages : 1482 pages
Book Rating : 4.:/5 (891 download)

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Book Synopsis Monthly Catalog of United States Government Publications by :

Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1995 with total page 1482 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Stability and Control/wind Tunnel Data Correlation

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ISBN 13 :
Total Pages : 224 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Aerodynamic Stability and Control/wind Tunnel Data Correlation by : G. R. Casteel

Download or read book Aerodynamic Stability and Control/wind Tunnel Data Correlation written by G. R. Casteel and published by . This book was released on 1971 with total page 224 pages. Available in PDF, EPUB and Kindle. Book excerpt: The general objective was to collect and analyze aerodynamic stability and control data for the XV-4B, XV-5A, and P-1127 VTOL configurations. Correlation and analysis of existing model data were made to investigate hover and transition characteristics. Particular emphasis was placed on the aerodynamic power effects, sometimes referred to as interference effects. Other areas of investigation were sometimes referred to as interference effects. Other areas of investigation were nondimensional coefficients used to present VTOL data and wind tunnel test techniques. Wind tunnel tests were conducted using an inlet only model and a jet only model to investigate special test and analysis problems for these components. The agreement between different sets of XV-4B model data was, in general, found to be poor. However, the nondimensional coefficients used by Lockheed to reduce to XV-4B model data appear to be valid parameters for this category of VTOL airplane. The jet entrainment flow was shown by experiment to be the primary cause of the XV-4B power effects, and the XV-4B jet path was experimentally and theoretically determined.

Government Reports Announcements & Index

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ISBN 13 :
Total Pages : 1194 pages
Book Rating : 4.3/5 (91 download)

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Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1995 with total page 1194 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Recent Advances in Aerodynamics

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Publisher : Springer Science & Business Media
ISBN 13 : 1461249724
Total Pages : 752 pages
Book Rating : 4.4/5 (612 download)

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Book Synopsis Recent Advances in Aerodynamics by : Anjaneyulu Krothapalli

Download or read book Recent Advances in Aerodynamics written by Anjaneyulu Krothapalli and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 752 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Joint Institute for Aeronautics and Acoustics at Stanford University was established in October 1973 to provide an academic environment for long-term cooperative research between Stanford and NASA Ames Research Center. Since its establishment, the In stitute has wnducted theoretical and experimental work in the areas of aerodynamics, acoustics, fluid mechanics, flight dynamics, guid ance and control, and human factors. This research has involved Stanford faculty, research associates, graduate students, and many distinguished visitors in collaborative efforts with the research staff of NASA Ames Research Center. The occasion of the Institute's tenth anniversary was used to reflect back on where that research has brought us, and to consider where our endeavors should be directed next. Thus, an International Symposium was held to review recent advances in the fields relevant to the activities of the Institute and to discuss the areas of research to be undertaken in the future. This anniversary was also chosen a.."1 an opportunity to honor one of the Institute's founders and its di rector, Professor Krishnamurty Karamcheti. It has been his creative inspiration that has provided the ideal research environment at the Joint Institute. The International Symposium on Recent Advances in Aero dynamics and Aconstics was held at Stanford University, Stanford, California, U.S.A., August 22-26, 198:~. Thirty-five distinguished scientists were invited to present a comprehensive review on the fol lowing subject areas: unsteady aerodynamics, jets and shear layers, V /STOL aircraft aerodynamics, rotor dynamics and aerodynamics,.

Summary of In-flight Flow Visualization Obtained from the NASA High Alpha Research Vehicle

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ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Summary of In-flight Flow Visualization Obtained from the NASA High Alpha Research Vehicle by : David F. Fisher

Download or read book Summary of In-flight Flow Visualization Obtained from the NASA High Alpha Research Vehicle written by David F. Fisher and published by . This book was released on 1991 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flow Visualization Studies of the XFV-12A.

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Flow Visualization Studies of the XFV-12A. by : Charles Lewis Peterson

Download or read book Flow Visualization Studies of the XFV-12A. written by Charles Lewis Peterson and published by . This book was released on 1975 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The XFV-12A incorporates thrust augmentation to generate propulsive lift. Under the influence of forward flight the lift jets are subject to bending, which produces shed vortices that induce velocities at the aircraft. Additionally, operations in ground effect during hover and for small forward velocities can result in reingestion of engine exhaust gases. The objectives of this thesis were twofold. The first was to investigate analytically aspects of the vortex shedding phenomenon through the application of potential flow around the lifting surfaces of the aircraft. Secondly, experimental analysis was performed to determine the unique reingestion properties of the XFV-12A operating statically under various wing and canard configurations.

Effects of Lateral Control Characteristics on Hovering a Jet Lift VTOL Aircraft

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ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effects of Lateral Control Characteristics on Hovering a Jet Lift VTOL Aircraft by : L. Stewart Rolls

Download or read book Effects of Lateral Control Characteristics on Hovering a Jet Lift VTOL Aircraft written by L. Stewart Rolls and published by . This book was released on 1965 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 325)

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ISBN 13 :
Total Pages : 470 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 325) by :

Download or read book Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 325) written by and published by . This book was released on 1995 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic and Related Hydrodynamic Studies Using Water Facilities

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ISBN 13 :
Total Pages : 484 pages
Book Rating : 4.:/5 (359 download)

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Book Synopsis Aerodynamic and Related Hydrodynamic Studies Using Water Facilities by : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium

Download or read book Aerodynamic and Related Hydrodynamic Studies Using Water Facilities written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium and published by . This book was released on 1987 with total page 484 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Model Tests of Jet-induced Lift Effects on a VTOL Aircraft in Hover

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ISBN 13 :
Total Pages : 140 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Model Tests of Jet-induced Lift Effects on a VTOL Aircraft in Hover by : P. K. Shumpert

Download or read book Model Tests of Jet-induced Lift Effects on a VTOL Aircraft in Hover written by P. K. Shumpert and published by . This book was released on 1969 with total page 140 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aeronautical Engineering

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ISBN 13 :
Total Pages : 580 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Aeronautical Engineering by :

Download or read book Aeronautical Engineering written by and published by . This book was released on 1971 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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)

Hover In-ground-effect Testing of a Full-scale, Tilt-nacelle V/STOL Model

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Hover In-ground-effect Testing of a Full-scale, Tilt-nacelle V/STOL Model by :

Download or read book Hover In-ground-effect Testing of a Full-scale, Tilt-nacelle V/STOL Model written by and published by . This book was released on 1986 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: