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Book Boundary layer Equations and Their Boundary Conditions in the Case of Motion at Supersonic Velocities in a Moderately Rarefied Gas

Download or read book Boundary layer Equations and Their Boundary Conditions in the Case of Motion at Supersonic Velocities in a Moderately Rarefied Gas written by I︠U︡. N. Lunkin and published by . This book was released on 1960 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Boundary layer Equations and Their Boundary Conditions in the Case of Motion at Supersonic Velocities in a Moderately Rarefied Gas

Download or read book Boundary layer Equations and Their Boundary Conditions in the Case of Motion at Supersonic Velocities in a Moderately Rarefied Gas written by I︠U︡. N. Lunkin and published by . This book was released on 1960 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Boundary layer Equations and Their Boundary Conditions in Case of Motion at Supersonic Velocities in Moderately Rarefied Gas  with List of Literature Cited

Download or read book Boundary layer Equations and Their Boundary Conditions in Case of Motion at Supersonic Velocities in Moderately Rarefied Gas with List of Literature Cited written by and published by . This book was released on 1960 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Boundary Layer Equations and Boundary Conditions for Them in the Case of Motion in a Slightly Rarefied Gas with Supersonic Speeds

Download or read book Boundary Layer Equations and Boundary Conditions for Them in the Case of Motion in a Slightly Rarefied Gas with Supersonic Speeds written by Yu P. Lun'kin and published by . This book was released on 1964 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: By using Prandtl's boundary-layer theory, equations are derived for a moderately rarefied gas which differ from the ordinary Prandtl equations by the presence of supplementary terms that contain higher derivatives of velocity and temperature; in the equations derived, the normal pressure gradient differs from zero and is expressed by supplementary terms. The boundary conditions for these equations are found with the aid of kinetic theory; they are a generalization of Maxwell's and Smoluchowski's conditions for motion at a supersonic velocity. The velocity and height limits of applicability of the equations derived are set forth. (Author).

Book NASA Technical Translation

Download or read book NASA Technical Translation written by and published by . This book was released on 1960 with total page 384 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book U S  Government Research Reports

Download or read book U S Government Research Reports written by and published by . This book was released on 1964 with total page 1118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of NACA Technical Publications

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 860 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of NASA Technical Publications

Download or read book Index of NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1970 with total page 772 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index of NASA Technical Publications

Download or read book Index of NASA Technical Publications written by and published by . This book was released on 1959 with total page 494 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Translations

Download or read book Technical Translations written by and published by . This book was released on 1960 with total page 722 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Selected Listing of NASA Scientific and Technical Reports for

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1959 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Index to NASA Technical Publications

Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Journal of the Royal Aeronautical Society

Download or read book Journal of the Royal Aeronautical Society written by Royal Aeronautical Society and published by . This book was released on 1962 with total page 1164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Bibliography of Scientific and Industrial Reports

Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1970-05 with total page 1006 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Science Abstracts

Download or read book Science Abstracts written by and published by . This book was released on 1961 with total page 932 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Stagnation point Flow of a Variable property Fluid at Low Reynolds Numbers

Download or read book Stagnation point Flow of a Variable property Fluid at Low Reynolds Numbers written by Michael Lenard and published by . This book was released on 1962 with total page 360 pages. Available in PDF, EPUB and Kindle. Book excerpt: Steady, viscous, two-dimensional and axially symmetric stagnation-point flows of a gas are considered for the case when the Reynolds number is too low for the applicability of the classical boundary-layer theory. It is assumed that the low-density gas is still a continuous fluid, permitting the use of the Navier-Stokes and as associated equations as the basis of the problem. The effects of low Reynolds number are determined by applying an expansion procedure to the fluid dynamical equations.