Nol Hypersonic Tunnel
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| Author | : James E. Danberg |
| Publisher | : |
| Total Pages | : 84 |
| Release | : 1964 |
| Genre | : Hypersonic wind tunnels |
| ISBN | : |
NOL's Hypersonic Tunnel No. 4 is a continuous blow-down hypersonic tunnel designed for research and development testing of models, instrumentation, and wind tunnel components. It can operate at Mach numbers from 5 to 10 with supply pressures up to 52 atmospheres and supply temperatures up to 1700 R. This report summarizes the pertinent aerodynamic design criteria and operating experience compiled during its first eleven years of operation. Included are descriptions of the major components and their performance along with the flight simulation capability of the facility and a bibliography of previously published reports. (Author).
| Author | : Frank P. Baltakis |
| Publisher | : |
| Total Pages | : 146 |
| Release | : 1968 |
| Genre | : Hypersonic wind tunnels |
| ISBN | : |
The report summarizes the performance capability data of the U.S. Naval Ordnance Laboratory's Hypersonic Tunnel. The report includes a brief description of the facility, overall performance capability data, nozzle calibration data, and some nozzle boundary-layer thickness and temperature variation data. The nozzle aerodynamic design method is indicated and its adequacy in the range of the supply and test flow conditions of the Hypersonic Tunnel is briefly discussed. (Author).
| Author | : Albert L. Braslow |
| Publisher | : |
| Total Pages | : 624 |
| Release | : 1958 |
| Genre | : Airplanes |
| ISBN | : |
The method has been applied to various types of configurations in several wind-tunnel investigations conducted by the National Advisory Committee for Aeronautics at Mach numbers up to 4, and in all cases the calculated roughness height caused premature boundary-layer transition for the range of test conditions.
| Author | : United States. National Advisory Committee for Aeronautics |
| Publisher | : |
| Total Pages | : 690 |
| Release | : 1958 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 694 |
| Release | : 1949 |
| Genre | : Science |
| ISBN | : |
| Author | : Johns Hopkins University. Applied Physics Laboratory |
| Publisher | : |
| Total Pages | : 364 |
| Release | : 1966 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 424 |
| Release | : 1971 |
| Genre | : |
| ISBN | : |
| Author | : Peter O. K. Krehl |
| Publisher | : Springer Science & Business Media |
| Total Pages | : 1298 |
| Release | : 2008-09-24 |
| Genre | : Science |
| ISBN | : 3540304215 |
This unique and encyclopedic reference work describes the evolution of the physics of modern shock wave and detonation from the earlier and classical percussion. The history of this complex process is first reviewed in a general survey. Subsequently, the subject is treated in more detail and the book is richly illustrated in the form of a picture gallery. This book is ideal for everyone professionally interested in shock wave phenomena.
| Author | : |
| Publisher | : |
| Total Pages | : 744 |
| Release | : 1958 |
| Genre | : Science |
| ISBN | : |
| Author | : Zonglin Jiang |
| Publisher | : Cambridge University Press |
| Total Pages | : 315 |
| Release | : 2023-10-26 |
| Genre | : Technology & Engineering |
| ISBN | : 131651675X |
A comprehensive reference on the basics, physics, design methods, and testing of various state-of-the art hypervelocity shock tunnels.
