Author: Milt DavisPublisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, Jun 7-Jun 10, 1999.
A proposal for integration of wind tunnel and engine test programs for the evaluation of airframe-propulsion compatibility using numerical simulations, ASME 99-GT-345
Author: Milt DavisPublisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Indianapolis, Indiana, Jun 7-Jun 10, 1999.
A Proposal for Integration of Wind Tunnel and Engine Test Programs for the Evaluation of Airframe-propulsion Compatibility Using Numerical Simulations
Author: Milt DavisPublisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 0
Book Description
ASME Technical Papers
Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 438
Book Description
Paper
Author: Publisher:
ISBN:
Category : Mechanical engineering
Languages : en
Pages : 452
Book Description
Journal of Engineering for Gas Turbines and Power
Author: Full Scale Subsonic Wind Tunnel Requirements and Design Studies
Author: Mark W. KellyWind Tunnel/flight Data Correlation (u).
Author: James A. BehalPublisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 692
Book Description
A program was conducted to obtain data, both steady state and dynamic, from wind tunnel models and full scale flight tests of the RA-5C aircraft. Data were acquired on 0.228 and 0. 125 scale RA-5C inlet models and on a fully instrumented flight test RA-5C aircraft. Interim data reports presenting the data acquired during each test have been published. These data were utilized in this report to develop scaling techniques for correlating small scale model wind tunnel data with full scale flight data. Data presented include duct steady state operating characteristics and pressure distributions in the inlet and at the engine face. Dynamic data are presented in the form of engine face turbulence contour plots, radial turbulence distributions and selected spectral data functions. Data are presented for variations of angle of attack, angle of yaw, Reynolds number, ramp angle, secondary flow rates and inlet diverter width. Brief descriptions of the model and test methods are also presented.
Wind Tunnel Test Techniques
Author: Colin BritcherPublisher: Academic Press
ISBN: 0128181001
Category : Technology & Engineering
Languages : en
Pages : 672
Book Description
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
Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel
Author: Richard P. KrebsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 34
Book Description
Author: Jean-Claude Raynal