A Wind Tunnel Investigation Of Effects Of Noise Bluntness Face Shape And Afterbody Length On The Aerodynamic Characteristics Of Bodies Of Revolution At Mach Numbers Of 2 37 2 98 And 3 90

A Wind Tunnel Investigation Of Effects Of Noise Bluntness Face Shape And Afterbody Length On The Aerodynamic Characteristics Of Bodies Of Revolution At Mach Numbers Of 2 37 2 98 And 3 90 Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of A Wind Tunnel Investigation Of Effects Of Noise Bluntness Face Shape And Afterbody Length On The Aerodynamic Characteristics Of Bodies Of Revolution At Mach Numbers Of 2 37 2 98 And 3 90 book. This book definitely worth reading, it is an incredibly well-written.

Convective Heat Transfer in Planetary Gases

Author : Joseph G. Marvin,George S. Deiwert
Publisher : Unknown
Page : 60 pages
File Size : 51,5 Mb
Release : 1965
Category : Heat
ISBN : UIUC:30112106681593

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Convective Heat Transfer in Planetary Gases by Joseph G. Marvin,George S. Deiwert Pdf

Equilibrium convective heat transfer in several real gases was investigated. The gases considered were air, nitrogen, hydrogen, carbon dioxide, and argon. Solutions to the similar form of the boundary-layer equations were obtained for flight velocities to 30,000 ft/sec for a range of parameters sufficient to define the effects of pressure level, pressure gradient, boundary-layer-edge velocity, and wall temperature. Results are presented for stagnation-point heating and for the heating-rate distribution. For the range of parameters investigated the wall heat transfer depended on the transport properties near the wall and precise evaluation of properties in the high-energy portions of the boundary layer was not needed. A correlation of the solutions to the boundary-layer equations was obtained which depended only on the low temperature properties of the gases. This result can be used to evaluate the heat transfer in gases other than those considered. The largest stagnation-point heat transfer at a constant flight velocity was obtained for argon followed successively by carbon dioxide, air, nitrogen, and hydrogen. The blunt-body heating-rate distribution was found to depend mainly on the inviscid flow field. For each gas, correlation equations of boundary-layer thermodynamic and transport properties as a function of enthalpy are given for a wide range of pressures to a maximum enthalpy of 18,000 Btu/lb.

The Blunt Plate in Hypersonic Flow

Author : Donald Louis Baradell,Mitchel H. Bertram
Publisher : Unknown
Page : 54 pages
File Size : 47,8 Mb
Release : 1960
Category : Fluid mechanics
ISBN : UIUC:30112106689349

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The Blunt Plate in Hypersonic Flow by Donald Louis Baradell,Mitchel H. Bertram Pdf

High-speed Wind Tunnels

Author : Luigi Crocco
Publisher : Unknown
Page : 230 pages
File Size : 55,5 Mb
Release : 1946
Category : Aerodynamics, Supersonic
ISBN : CORNELL:31924004607473

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High-speed Wind Tunnels by Luigi Crocco Pdf

The importance assumed in recent times by experimental supersonic wind tunnels, as well as the power required, has brought about the need for a study which would permit a comparison of the types tested and the principal theoretical plans.

Facing the Heat Barrier

Author : T. A. Heppenheimer
Publisher : Unknown
Page : 364 pages
File Size : 50,5 Mb
Release : 2006
Category : Science
ISBN : PURD:32754079096438

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Facing the Heat Barrier by T. A. Heppenheimer Pdf

Hypersonics is the study of flight at speeds where aerodynamic heating dominates the physics of the problem. Typically this is Mach 5 and higher. Hypersonics is an engineering science with close links to supersonics and engine design. Within this field, many of the most important results have been experimental. The principal facilities have been wind tunnels and related devices, which have produced flows with speeds up to orbital velocity. Why is it important? Hypersonics has had two major applications. The first has been to provide thermal protection during atmospheric entry. Success in this enterprise has supported ballistic-missile nose cones, has returned strategic reconnaissance photos from orbit and astronauts from the Moon, and has even dropped an instrument package into the atmosphere of Jupiter. The last of these approached Jupiter at four times the speed of a lunar mission returning to Earth. Work with re-entry has advanced rapidly because of its obvious importance. The second application has involved high-speed propulsion and has sought to develop the scramjet as an advanced airbreathing ramjet. Scramjets are built to run cool and thereby to achieve near-orbital speeds. They were important during the Strategic Defense Initiative, when a set of these engines was to power the experimental X-30 as a major new launch vehicle. This effort fell short, but the X-43A, carrying a scramjet, has recently flown at Mach 9.65 by using a rocket. Atmospheric entry today is fully mature as an engineering discipline. Still, the Jupiter experience shows that work with its applications continues to reach for new achievements. Studies of scramjets, by contrast, still seek full success, in which such engines can accelerate a vehicle without the use of rockets. Hence, there is much to do in this area as well. For instance, work with computers may soon show just how good scramjets can become. NASA SP-2007-4232

Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles

Author : Gino Sovran
Publisher : Springer Science & Business Media
Page : 381 pages
File Size : 51,8 Mb
Release : 2012-12-06
Category : Technology & Engineering
ISBN : 9781468484342

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Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles by Gino Sovran Pdf

These Proceedings contain the papers and oral discussions presented at the Symposium on AERODYNAMIC DRAG MECHANISMS of Bluff Bodies and Road Vehides held at the General Motors Research Laboratories in Warren, Michigan, on September 27 and 28, 1976. This international, invitational Symposium was the twentieth in an annual series, each one having been in a different technical discipline. The Symposia provide a forum for areas of science and technology that are of timely interest to the Research Laboratories as weIl as the technical community at large, and in which personnel of the Laboratories are actively involved. The Symposia furnish an opportunity for the exchange of ideas and current knowledge between participating research specialists from educational, industrial arid governmental institutions and serve to stimulate future research activity. The present world-wide energy situation makes it highly desirable to reduce the force required to move road vehicles through the atmosphere. A significant amount of the total energy consumed for transportation is expended in overcoming the aerodynamic resistance to motion of these vehicles. Reductions in this aerodynamic drag can therefore have a large impact on ground transportation energy requirements. Although aerodynamic development work on road vehides has been performed for many years, it has not been widely reported or accompanied by much basic research.

Innovation in Flight

Author : Joseph R. Chambers
Publisher : Unknown
Page : 406 pages
File Size : 52,7 Mb
Release : 2005
Category : Aeronautics
ISBN : IND:30000109243109

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Innovation in Flight by Joseph R. Chambers Pdf

Beyond Tube-and-Wing

Author : Bruce Larrimer
Publisher : Unknown
Page : 128 pages
File Size : 50,7 Mb
Release : 2020-06-15
Category : Electronic
ISBN : 1626830592

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Beyond Tube-and-Wing by Bruce Larrimer Pdf

Aerodynamics of Space Vehicles

Author : Anonim
Publisher : Unknown
Page : 68 pages
File Size : 50,9 Mb
Release : 1963
Category : Aerodynamics
ISBN : STANFORD:36105113725910

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Aerodynamics of Space Vehicles by Anonim Pdf

Handbook of Supersonic Aerodynamics

Author : Johns Hopkins University. Applied Physics Laboratory,Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Publisher : Unknown
Page : 428 pages
File Size : 49,6 Mb
Release : 1950
Category : Aerodynamics, Supersonic
ISBN : UOM:39015047367712

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Handbook of Supersonic Aerodynamics by Johns Hopkins University. Applied Physics Laboratory,Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md Pdf

Transonic Wind Tunnel Testing

Author : B. H. Goethert
Publisher : Unknown
Page : 420 pages
File Size : 42,5 Mb
Release : 2007
Category : Science
ISBN : UVA:X030260513

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Transonic Wind Tunnel Testing by B. H. Goethert Pdf

Numerous aspects of transonic aerodynamics include wall interference corrections in conventional wind tunnels, subsonic flow in a variety of wind tunnels, and test results from transonic wind tunnels. 1961 edition.

An Investigation of a Device to Oscillate a Wind-tunnel Airstream

Author : Charles F. Reid,Clifton Wrestler (G.)
Publisher : Unknown
Page : 36 pages
File Size : 54,5 Mb
Release : 1961
Category : Oscillations
ISBN : UIUC:30112106682161

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An Investigation of a Device to Oscillate a Wind-tunnel Airstream by Charles F. Reid,Clifton Wrestler (G.) Pdf

Design and Development of Aerospace Vehicles and Propulsion Systems

Author : S. Kishore Kumar,Indira Narayanaswamy,V. Ramesh
Publisher : Springer Nature
Page : 529 pages
File Size : 54,8 Mb
Release : 2021-03-18
Category : Technology & Engineering
ISBN : 9789811596018

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Design and Development of Aerospace Vehicles and Propulsion Systems by S. Kishore Kumar,Indira Narayanaswamy,V. Ramesh Pdf

This book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India), Gas-Turbine Research Establishment (responsible for design and development of gas turbine engines for military applications), and CSIR-National Aerospace Laboratories (involved in major aerospace programs in the country such as SARAS program, LCA, Space Launch Vehicles, Missiles and UAVs). It brings together experiences of aerodynamicists in India as well as abroad in Aerospace Vehicle Design, Gas Turbine Engines, Missiles and related areas. It is a useful volume for researchers, professionals and students interested in diversified areas of aerospace engineering.

Intelligence Revolution 1960

Author : Ingard Clausen,Edward A. Miller
Publisher : Unknown
Page : 260 pages
File Size : 46,8 Mb
Release : 2012
Category : Astronautics, Military
ISBN : UCBK:C083580642

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Intelligence Revolution 1960 by Ingard Clausen,Edward A. Miller Pdf

Overview: Provides a history of the Corona Satellite photo reconnaissance Program. It was a joint Central Intelligence Agency and United States Air Force program in the 1960s. It was then highly classified.