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Author : K.R. Enkenhus
Publisher :
ISBN 13 :
Total Pages : 61 pages
Book Rating : 4.:/5 (11 download)
Download or read book Aerodynamic Design of a Continous Hypervelocity Wind Tunnel written by K.R. Enkenhus and published by . This book was released on 1962 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Naval Ordnance Laboratory (White Oak, Md.).
Publisher :
ISBN 13 :
Total Pages : 92 pages
Book Rating : 4.3/5 (91 download)
Download or read book NOL Hypervelocity Wind Tunnel: Aerodynamic design written by Naval Ordnance Laboratory (White Oak, Md.). and published by . This book was released on 1971 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : K. R. ENKENHUS
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (227 download)
Download or read book Aerodynamic Design of a Continuous Hypervelocity Wind Tunnel written by K. R. ENKENHUS and published by . This book was released on 1962 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: A N AERO YNA IC DESIGN STUDY WAS MADE OF A CONTINUOUS, HYPERVELOCI Y IND TU NEL FOR SIMUL I G T E FLIGHT ENVIRONMENT OF LONG-RANGE BALLISTIC MISSILES ND GLIDE V ICLES AT Mach numbers up to 20. Nozzles were designed by the m tho of characteristics for high-temperature air in dissociative and vibrational equilibrium. Since non-equilibriu flow was e pected to occur under many conditions, the effect of a fi ite O r co binatio r te on the flow in hyper onic nozzles was determine for a wide rang of supply conditions. The nozzle turbulent boundary-layer growth and heat ransfer were calculated by a mome tum-integral method e ployi g thermody amic and ransport properties appropriate to hig -temper ure air. The extremely high he t-transf r r tes near the nozzle throat create a severe cooling problem B OTH CONVECTIVE COOLING, USING WATER OR LIQUID METALS, AND FILM COOLING, WITH AIR OR WATER I J CTION RE STUDIED. The application of the electric arc as an air ea ing devic, nd the performance of a hypersonic diffuser were also examined Conclusions re drawn from the resul s of this s udy regarding the range of free-flig t condi io s which can be simul d in the wind unnel. (Author).
Author : Colin Britcher
Publisher : Academic Press
ISBN 13 : 0128181001
Total Pages : 672 pages
Book Rating : 4.1/5 (281 download)
Download or read book Wind Tunnel Test Techniques written by Colin Britcher and published by Academic Press. This book was released on 2023-10-20 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Wind Tunnel Test Techniques: Design and Use at Low and High Speeds with Statistical Engineering Applications provides an up-to-date treatment of the topic. Beginning with a brief history of wind tunnels and its types and uses, the book goes on to cover subsonic, supersonic and hypersonic wind tunnel design and construction, calibration, boundary corrections, flow quality assessment, pressure surveys, and dynamic testing. It also focuses on wind tunnel facilities, making it useful for both the designer and operator. Engineers and graduate students in aerospace, automotive and similar programs will find this book useful in their work with experimental aerodynamics, gas dynamics, facility design and performance. - Deals with a broad range of flow speeds in wind tunnels, from low speed to high speed - Provides a discussion of similarity laws as well as material on statistical analysis - Includes coverage on facility-to-facility and facility-to-CFD correlation - Presents advanced topics such as cryogenic wind tunnels, ground simulation in automotive testing, and propulsion testing
Author : J. C. Sivells
Publisher :
ISBN 13 :
Total Pages : 152 pages
Book Rating : 4.:/5 (227 download)
Download or read book A Computer Program for the Aerodynamic Design of Axisymmetric and Planar Nozzles for Supersonic and Hypersonic Wind Tunnels written by J. C. Sivells and published by . This book was released on 1978 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computer program is presented for the aerodynamic design of axisymmetric and planar nozzles for supersonic and hypersonic wind tunnels. The program is the culmination of the effort expended at various times over a number of years to develop a method of designing a wind tunnel with an inviscid contour which has continuous curvature and which is corrected for the growth of the boundary layer in a manner such that uniform parallel flow can be expected at the nozzle exit. The continuous curvature is achieved through specification of a centerline distribution of velocity (or Mach number) which has first and second derivatives that (1) are compatible with a transonic solution near the throat and with radial flow near the inflection point and (2) approach zero at the design Mach number. The boundary-layer growth is calculated by solving a momentum integral equation by numerical integration.
Author : Harris M. Schurmeier
Publisher :
ISBN 13 :
Total Pages : 304 pages
Book Rating : 4.3/5 (91 download)
Download or read book Design and Operation of a Continuous-flow Hypersonic Wind Tunnel Using a Two-dimensional Nozzle written by Harris M. Schurmeier and published by . This book was released on 1959 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James C. Sivells
Publisher :
ISBN 13 :
Total Pages : 57 pages
Book Rating : 4.:/5 (423 download)
Download or read book Aerodynamic Design and Calibration of the Vkf 50-inch Hypersonic Wind Tunnels written by James C. Sivells and published by . This book was released on 1963 with total page 57 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H. M. Schurmeier
Publisher :
ISBN 13 :
Total Pages : 156 pages
Book Rating : 4.:/5 (633 download)
Download or read book Design and Operation of a Continous-flow Hypersonic Wind Tunnel Using a Two-dimensional Nozzle written by H. M. Schurmeier and published by . This book was released on 1959 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium
Publisher :
ISBN 13 :
Total Pages : 452 pages
Book Rating : 4.E/5 ( download)
Download or read book Aerodynamics of Wind Tunnel Circuits and Their Components written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium and published by . This book was released on 1997 with total page 452 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Naval Ordnance Laboratory (White Oak, Md.).
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.3/5 (91 download)
Download or read book NOL Hypervelocity Wind Tunnel written by Naval Ordnance Laboratory (White Oak, Md.). and published by . This book was released on 1971 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James E. Danberg
Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.3/5 (91 download)
Download or read book NOL Hypersonic Tunnel No. 4 written by James E. Danberg and published by . This book was released on 1964 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 : Ruth N. Weitmann
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Design and Calibration of an Arc-heated, Hypersonic, Low-density Wind Tunnel written by Ruth N. Weitmann and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Noor Ahmed
Publisher : BoD – Books on Demand
ISBN 13 : 9535110470
Total Pages : 232 pages
Book Rating : 4.5/5 (351 download)
Download or read book Wind Tunnel Designs and Their Diverse Engineering Applications written by Noor Ahmed and published by BoD – Books on Demand. This book was released on 2013-03-06 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is intended to be a valuable addition to students, engineers, scientists, industrialists, consultants and others providing greater insight into wind tunnel designs and their enormous research potential. It is a compilation of works from world experts on subsonic and supersonic wind tunnel designs, applicable to a diverse range of disciplines. The book is organised in two sections. The first section comprises of three chapters on various aspects of stationary and portable subsonic wind tunnel designs, followed by one chapter on supersonic wind tunnel and the final chapter discusses a method to address unsteadiness effects of fan blade rotation. The second section contains four chapters regarding wind tunnel applications across a multitude of engineering fields including civil, mechanical, chemical and environmental engineering.
Author : Michael Witunski
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (287 download)
Download or read book The Aerodynamic Design and Instrumentation of a Supersonic Wind Tunnel written by Michael Witunski and published by . This book was released on 1948 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Vernon Parker Roan
Publisher :
ISBN 13 :
Total Pages : 364 pages
Book Rating : 4.:/5 (133 download)
Download or read book The Aerodynamic Design of a 5x7 Foot Subsonic Wind Tunnel for the University of Florida written by Vernon Parker Roan and published by . This book was released on 1959 with total page 364 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Bhaskar Bhatnagar
Publisher :
ISBN 13 :
Total Pages : 174 pages
Book Rating : 4.:/5 (558 download)
Download or read book Aerodynamic Design of a Wind Tunnel Inlet for Testing Class-8 Trucks written by Bhaskar Bhatnagar and published by . This book was released on 2003 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Luigi Crocco
Publisher :
ISBN 13 :
Total Pages : 236 pages
Book Rating : 4.E/5 ( download)
Download or read book High-speed Wind Tunnels written by Luigi Crocco and published by . This book was released on 1946 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.
