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Theory Of Thin Wing In A Supersonic Flow With Consideration Of The Non Equilibrium State Of Excitation Of Oscillating Degrees Of Freedom
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Book Synopsis Theory of Thin Wing in a Supersonic Flow with Consideration of the Non-Equilibrium State of Excitation of Oscillating Degrees of Freedom by : Ye P. Aksenov
Download or read book Theory of Thin Wing in a Supersonic Flow with Consideration of the Non-Equilibrium State of Excitation of Oscillating Degrees of Freedom written by Ye P. Aksenov and published by . This book was released on 1978 with total page 18 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 1979 with total page 738 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 Technical Abstract Bulletin written by and published by . This book was released on with total page 1048 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP. written by and published by . This book was released on 1993 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1979 with total page 1414 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1993 with total page 932 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).
Book Synopsis Government reports annual index by :
Download or read book Government reports annual index written by and published by . This book was released on 199? with total page 906 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Two-dimensional Wing Theory in the Supersonic Range by : H. Hönl
Download or read book Two-dimensional Wing Theory in the Supersonic Range written by H. Hönl and published by . This book was released on 1949 with total page 764 pages. Available in PDF, EPUB and Kindle. Book excerpt: The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.
Book Synopsis Wing Theory in Supersonic Flow by : Elie Carafoli
Download or read book Wing Theory in Supersonic Flow written by Elie Carafoli and published by Pergamon. This book was released on 1969 with total page 618 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Theory of Thin Wings in Subsonic Flow by : Sergeǐ Mikhaǐlovich Belotserkovskiǐ
Download or read book The Theory of Thin Wings in Subsonic Flow written by Sergeǐ Mikhaǐlovich Belotserkovskiǐ and published by Springer. This book was released on 2013-12-11 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Two-dimensional Wing Theory in the Supersonic Range by : H. Honl
Download or read book Two-dimensional Wing Theory in the Supersonic Range written by H. Honl and published by . This book was released on 1947 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt: The plane problem of the vibrating wing in supersonic flow is discussed and followed by the acceleration potential method, on the basis of a linearized theory.
Book Synopsis Theoretical Studies of Supersonic Two-dimensional and Axisymmetric Nonequilibrium Flow, Including Calculations of Flow Through a Nozzle by : James Joe Der
Download or read book Theoretical Studies of Supersonic Two-dimensional and Axisymmetric Nonequilibrium Flow, Including Calculations of Flow Through a Nozzle written by James Joe Der and published by . This book was released on 1963 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Chemical and vibrational nonequilibrium phenomena in steady inviscid flow fields are studied by the analysis of flow past curved boundaries. Possible alternative choices of the state variables to be used are considered. General features of the nonequilibrium flow are studied by examination of the mathematical properties of the nonlinear flow equations. An axisymmetric nonequilibrium flow of air through a supersonic nozzle is analyzed by means of numerical computations. The coupling effects between nonuniformity (across a nozzle section) and nonequilibrium, not taken into account in the quasi-one-dimensional flow approximation, are revealed by the present analysis.
Book Synopsis The Potential Theory of Unsteady Supersonic Flow by : John Wilder Miles
Download or read book The Potential Theory of Unsteady Supersonic Flow written by John Wilder Miles and published by . This book was released on 1980 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Government Reports Annual Index: Keyword A-L by :
Download or read book Government Reports Annual Index: Keyword A-L written by and published by . This book was released on 1979 with total page 840 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Influence Coefficients for an Oscillating Finite Thin Wing in Supersonic Flow by : Ta Li
Download or read book Aerodynamic Influence Coefficients for an Oscillating Finite Thin Wing in Supersonic Flow written by Ta Li and published by . This book was released on 1956 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Second-Order Theory for a Thin Wing in Supersonic Flow with a Weak Spanwise Entropy Gradients by : PETER G. WILBY
Download or read book Second-Order Theory for a Thin Wing in Supersonic Flow with a Weak Spanwise Entropy Gradients written by PETER G. WILBY and published by . This book was released on 1961 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: The three-dimensional perturbation velocities over an infinite thin wing with a sharp leading edge in non-uniform supersonic flow are derived and used to investigate the second-order contribution to the pressure coefficient on a wing surface, due to a spanwise entropy gradient. Pressure distributions are calculated for a wedge section wing at various Mach numbers for probable values of entropy gradient. Results show that entropy gradient effects can be important. Procedure for application of the theory is given for the case of a wing situated behind the curved shock generated by a blunt nosed body. (Author).
Book Synopsis Theoretical Relations Between the Stability Derivatives of a Wing in Direct and in Reverse Supersonic Flow by : Sidney M. Harmon
Download or read book Theoretical Relations Between the Stability Derivatives of a Wing in Direct and in Reverse Supersonic Flow written by Sidney M. Harmon and published by . This book was released on 1949 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investivation is made for thin flate-plate wings for steady vertical and longitudinal motions, setady rolling and pitching, and motions in which the wing is accelerating uniformly in the vertical direction.
