Development of Transonic Wind Tunnel Testing Technique
Author : J. Lukasiewicz
Publisher :
Page : pages
File Size : 44,71 MB
Release : 1954
Category :
ISBN :
Author : J. Lukasiewicz
Publisher :
Page : pages
File Size : 44,71 MB
Release : 1954
Category :
ISBN :
Author : B. H. Goethert
Publisher :
Page : 420 pages
File Size : 11,21 MB
Release : 2007
Category : Science
ISBN :
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.
Author : Colin Britcher
Publisher : Academic Press
Page : 672 pages
File Size : 13,36 MB
Release : 2023-10-20
Category : Technology & Engineering
ISBN : 0128181001
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 : Alan Pope
Publisher :
Page : 164 pages
File Size : 48,18 MB
Release : 1961
Category : Wind tunnels
ISBN :
Air-flow measuring instruments, their use, and the manner of working up and presenting the data obtained when calibrating low-speed, nearsonic, transonic, supersonic, and hypersonic wind tunnels are discussed. (Author).
Author : ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France)
Publisher :
Page : 498 pages
File Size : 16,22 MB
Release : 1984
Category :
ISBN :
This meeting reviewed the current status of new wind tunnel facilities and gave a perspective of recent developments in testing techniques and fluid motion problems related to wind tunnel testing. It was organized in five sessions. The session on Facilities dealt almost exclusively with cryogenic wind tunnels. The National Transonic Facility is operational and valuable experience already has been gained, not only on operational aspects but also on model design. The major European countries are putting considerable effort into the joint European Transonic Wind Tunnel. The emphasis on cryogenics was again highlighted in the session on Fluid Motion Problems, addressing such areas as condensation and nonadiabatic wall effects, as well as model test results from a cryogenic facility. Flow quality was also given prominence. That conventional wind tunnels are still the backbone of the Testing Establishment was demonstrated in the three sessions of Testing Techniques. The presentations covered a large variety of topics including support interference, dynamic testing, inlet/engine/afterbody related testing, store separation, half-model testing technique, aero-acoustic measurements and wind tunnel-flight data comparisons.
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium
Publisher :
Page : 452 pages
File Size : 11,34 MB
Release : 1997
Category : Aerodynamics
ISBN :
Author : Bernhard Herman GOETHERT
Publisher :
Page : 397 pages
File Size : 10,13 MB
Release : 1961
Category : Transonic wind tunnels
ISBN :
Author : North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher :
Page : 1010 pages
File Size : 29,71 MB
Release : 1955
Category : Wind tunnel models
ISBN :
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
Publisher :
Page : 450 pages
File Size : 33,82 MB
Release : 1971
Category : Aerodynamics, Transonic
ISBN :
In September 1968, the FDP of AGARD held a specialists' meeting in Paris on transonic aerodynamics, in recognition of the fact that the absence of adequate theoretical methods and wind-tunnels of high enough Reynolds number had already led to costly shortcomings in the transonic performance of certain combat and transport aircraft. Since projected aerospace systems, military, civil and space-oriented, would involve flight at Reynolds number of up to 100 million, the FDP undertook an examination of the requirements of NATO nations for wind tunnel facilities for testing large models at high Reynolds numbers.
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
Page : 500 pages
File Size : 14,33 MB
Release : 1995
Category : Aerodynamics
ISBN :