Numerical Analysis Of Flow Properties About Blunt Bodies Moving At Supersonic Speeds In An Equilibrium Gas
Download Numerical Analysis Of Flow Properties About Blunt Bodies Moving At Supersonic Speeds In An Equilibrium Gas full books in PDF, epub, and Kindle. Read online free Numerical Analysis Of Flow Properties About Blunt Bodies Moving At Supersonic Speeds In An Equilibrium Gas ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Harvard Lomax |
Publisher | : |
Total Pages | : 96 |
Release | : 1964 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
Download Numerical Analysis of Flow Properties about Blunt Bodies Moving at Supersonic Speeds in an Equilibrium Gas Book in PDF, Epub and Kindle
Author | : Harvard Lomax |
Publisher | : |
Total Pages | : 79 |
Release | : 1964 |
Genre | : |
ISBN | : |
Download Numerical Analysis of Flow Properties about Blunt Bodies Moving at SUpersonic Speeds in an Equilibriumm Gas Book in PDF, Epub and Kindle
Author | : Jerry Curtis South |
Publisher | : |
Total Pages | : 66 |
Release | : 1968 |
Genre | : Mathematical models |
ISBN | : |
Download Calculation of Axisymmetric Supersonic Flow Past Blunt Bodies with Sonic Corners Book in PDF, Epub and Kindle
Author | : Roger M. Winebarger |
Publisher | : |
Total Pages | : 28 |
Release | : 1970 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Experimental Study of the Shock Wave Due to a Blunt Leading Edge in the Hypersonic Merged-flow Regime Book in PDF, Epub and Kindle
Author | : Paul W. Huber |
Publisher | : |
Total Pages | : 44 |
Release | : 1967 |
Genre | : Plasma frequencies |
ISBN | : |
Download Deduction of Reentry Plasma Properties about Manned Orbital Spacecraft from Radio Signal Attenuation Data Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 84 |
Release | : 1979 |
Genre | : Science |
ISBN | : |
Download NASA Technical Paper Book in PDF, Epub and Kindle
Author | : Richard W. Barnwell |
Publisher | : |
Total Pages | : 44 |
Release | : 1967 |
Genre | : Aerodynamics |
ISBN | : |
Download Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow Book in PDF, Epub and Kindle
The finite-difference method which Peter D. Lax developed for treating unsteady inviscid flow fields is used to study the transient flow in the shock layer of a sphere that has been struck by a normal shock wave. Transient flow of this sort is encountered when a shock tube is used as a supersonic wind tunnel. Time histories of the shock detachment distance and the stagnation-point pressure and tangential velocity gradient are presented for ranges of the incident-shock Mach number and the perfect-gas specific-heat ratio. These results show that the stagnation-point pressure approaches the steady value much more rapidly than the shock detachment distance. In general, the stagnation-point pressure but more rapidly than the shock detachment distance. As the specific-heat ratio is decreased and the incident-shock Mach number is increased, the variation of the velocity gradient with respect to the shock detachment distance becomes more nearly linear.
Author | : |
Publisher | : |
Total Pages | : 580 |
Release | : 1969 |
Genre | : Compressibility |
ISBN | : |
Download Compressible Turbulent Boundary Layers Book in PDF, Epub and Kindle
Author | : |
Publisher | : |
Total Pages | : 418 |
Release | : 1975 |
Genre | : |
ISBN | : |
Download NASA Technical Note Book in PDF, Epub and Kindle
Author | : Richard W. Barnwell |
Publisher | : |
Total Pages | : 88 |
Release | : 1969 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Download Inviscid Radiating Shock Layers about Spheres Traveling at Hyperbolic Speeds in Air Book in PDF, Epub and Kindle
Time-dependent finite-difference techniques are used to obtain numerical solutions for the problem of the inviscid flow of radiating equilibrium air past sphere traveling at hyperbolic speeds. The effects of absorption are included, and results are presented for both gray and nongray absorption coefficient models for spheres with different radii. It is shown that the nondimensional heat-flux distributions for the gray and nongray models are similar and that these distributions are weak functions of the radius of the sphere and the altitude and strong functions of the flight velocity.