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Separated Flow Over Bodies Of Revolution Using An Unsteady Discrete Vorticity Cross Wake
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Book Synopsis Separated Flow Over Bodies of Revolution Using an Unsteady Discretevorticity Cross Wake by : Purdue University. School of Aeronautics and Astronautics
Download or read book Separated Flow Over Bodies of Revolution Using an Unsteady Discretevorticity Cross Wake written by Purdue University. School of Aeronautics and Astronautics and published by . This book was released on 1974 with total page 89 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed to determine the flow field of a body of revolution in separated flow. The computer was used to integrate various solutions and solution properties of the sub-flow fields which made up the entire flow field without resorting to a finite difference solution to the complete Navier-Stokes equations. The technique entails the use of the unsteady cross flow analogy and a new solution to the two-dimensional unsteady separated flow problem based upon an unsteady, discrete-vorticity wake. Data for the forces and moments on aerodynamic bodies at low speeds and high angle of attack (outside the range of linear inviscid theories) such that the flow is substantially separated are produced which compare well with experimental data. In addition, three dimensional steady separated regions and wake vortex patterns are determined. The computer program developed to perform the numerical calculations is described. (NTRL site)
Book Synopsis Separated Flow Over Bodies of Revolution Using an Unsteady Discrete-vorticity Cross Wake by : F. J. Marshall
Download or read book Separated Flow Over Bodies of Revolution Using an Unsteady Discrete-vorticity Cross Wake written by F. J. Marshall and published by . This book was released on 1974 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed to determine the flow field of a body of revolution in separated flow. The computer was used to integrate various solutions and solution properties of the sub-flow fields which made up the entire flow field without resorting to a finite difference solution to the complete Navier-Stokes equations. The technique entails the use of the unsteady cross flow analogy and a new solution to the two-dimensional unsteady separated flow problem based upon an unsteady, discrete-vorticity wake. Data for the forces and moments on aerodynamic bodies at low speeds and high angle of attack (outside the range of linear inviscid theories) such that the flow is substantially separated are produced which compare well with experimental data. In addition, three dimensional steady separated regions and wake vortex patterns are determined. The computer program developed to perform the numerical calculations is described.
Book Synopsis Separated Flow Over Bodies of Revolution Using an Unsteady Discretevorticity Cross Wake by : F. J. Marshall
Download or read book Separated Flow Over Bodies of Revolution Using an Unsteady Discretevorticity Cross Wake written by F. J. Marshall and published by . This book was released on 1974 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed to determine the flow field of a body of revolution in separated flow. The computer was used to integrate various solutions and solution properties of the sub-flow fields which made up the entire flow field without resorting to a finite difference solution to the complete Navier-Stokes equations. The technique entails the use of the unsteady cross flow analogy and a new solution to the two-dimensional unsteady separated flow problem based upon an unsteady, discrete-vorticity wake. Data for the forces and moments on aerodynamic bodies at low speeds and high angle of attack (outside the range of linear inviscid theories) such that the flow is substantially separated are produced which compare well with experimental data. In addition, three dimensional steady separated regions and wake vortex patterns are determined. The computer program developed to perform the numerical calculations is described.
Book Synopsis Separated Flow Over Bodies of Revolution Using an Unsteady Discrete-vorticity Cross Wake. Part 2: Computer Program Description by :
Download or read book Separated Flow Over Bodies of Revolution Using an Unsteady Discrete-vorticity Cross Wake. Part 2: Computer Program Description written by and published by . This book was released on 1974 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1987 with total page 1390 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Download or read book NASA Technical Report written by and published by . This book was released on 1977 with total page 470 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis High Angle of Attack Aerodynamics by : Josef Rom
Download or read book High Angle of Attack Aerodynamics written by Josef Rom and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 408 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamics of aircraft at high angles of attack is a subject which is being pursued diligently, because the modern agile fighter aircraft and many of the current generation of missiles must perform well at very high incidence, near and beyond stall. However, a comprehensive presentation of the methods and results applicable to the studies of the complex aerodynamics at high angle of attack has not been covered in monographs or textbooks. This book is not the usual textbook in that it goes beyond just presenting the basic theoretical and experimental know-how, since it contains reference material to practical calculation methods and technical and experimental results which can be useful to the practicing aerospace engineers and scientists. It can certainly be used as a text and reference book for graduate courses on subjects related to high angles of attack aerodynamics and for topics related to three-dimensional separation in viscous flow courses. In addition, the book is addressed to the aerodynamicist interested in a comprehensive reference to methods of analysis and computations of high angle of attack flow phenomena and is written for the aerospace scientist and engineer who is familiar with the basic concepts of viscous and inviscid flows and with computational methods used in fluid dynamics.
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1980 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Collection of Technical Papers by :
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1980 with total page 688 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Subsonic Vortex Shedding from Forebodies with Chines by : M. R. Mendenhall
Download or read book Prediction of Subsonic Vortex Shedding from Forebodies with Chines written by M. R. Mendenhall and published by . This book was released on 1990 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Vortex Shedding from Circular and Noncircular Bodies in Supersonic Flow by : M. R. Mendenhall
Download or read book Prediction of Vortex Shedding from Circular and Noncircular Bodies in Supersonic Flow written by M. R. Mendenhall and published by . This book was released on 1984 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Tactical Missile Aerodynamics by : Michael J. Hemsch
Download or read book Tactical Missile Aerodynamics written by Michael J. Hemsch and published by . This book was released on 1986 with total page 890 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Contractor Report written by and published by . This book was released on 1990 with total page 558 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Review of Some Reynolds Number Effects Related to Bodies at High Angles of Attack by : Edward C. Polhamus (Jr.)
Download or read book A Review of Some Reynolds Number Effects Related to Bodies at High Angles of Attack written by Edward C. Polhamus (Jr.) and published by . This book was released on 1984 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Review of Some Reynolds Number Effects Related to Bodies at High Angles of Attack by : Edward C. Polhamus
Download or read book A Review of Some Reynolds Number Effects Related to Bodies at High Angles of Attack written by Edward C. Polhamus and published by . This book was released on 1984 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transactions of the Japan Society for Aeronautical and Space Sciences by : Nihon Kōkū Uchū Gakkai
Download or read book Transactions of the Japan Society for Aeronautical and Space Sciences written by Nihon Kōkū Uchū Gakkai and published by . This book was released on 1982 with total page 532 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Vortex Shedding from Circular and Noncircular Bodies in Subsonic Flow by : Michael R. Mendenhall
Download or read book Prediction of Vortex Shedding from Circular and Noncircular Bodies in Subsonic Flow written by Michael R. Mendenhall and published by . This book was released on 1987 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:
