Wind Tunnel Flight Data Correlation U
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Wind Tunnel Flight Data Correlation U
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Author : James A. Behal
language : en
Publisher:
Release Date : 1971
Wind Tunnel Flight Data Correlation U written by James A. Behal and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Buffeting (Aerodynamics) categories.
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 Flight Data Correlation U
DOWNLOAD
Author : James A. Behal
language : en
Publisher:
Release Date : 1971
Wind Tunnel Flight Data Correlation U written by James A. Behal and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Buffeting (Aerodynamics) categories.
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 Flight Data Correlation U
DOWNLOAD
Author : James A. Behal
language : en
Publisher:
Release Date : 1971
Wind Tunnel Flight Data Correlation U written by James A. Behal and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Buffeting (Aerodynamics) categories.
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.
A Correlation Between Flight Determined Derivatives And Wind Tunnel Data For The X 24b Research Aircraft
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Author :
language : en
Publisher:
Release Date : 1997
A Correlation Between Flight Determined Derivatives And Wind Tunnel Data For The X 24b Research Aircraft written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1997 with categories.
Wind Tunnel Flight Correlation Of Shock Induced Separated Flow
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Author : Donald L. Loving
language : en
Publisher:
Release Date : 1966
Wind Tunnel Flight Correlation Of Shock Induced Separated Flow written by Donald L. Loving and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1966 with Aerodynamic load categories.
Correlation Of Wind Tunnel And Flight Test Aerodynamic Data For Five V Stol Aircraft
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Author : David H. Hickey
language : en
Publisher:
Release Date : 1965
Correlation Of Wind Tunnel And Flight Test Aerodynamic Data For Five V Stol Aircraft written by David H. Hickey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1965 with Airplanes categories.
The five aircraft tested represent a wide variety of V/STOL concepts. Correlation between the wind-tunnel and flight-test aerodynamic results is generally good when wind-tunnel wall corrections are omitted; in some cases wall corrections are shown to degrade the correlation. The aircraft and wind-tunnel geometry are related to model-tunnel sizing parameters and a VTOL lift parameter, in order to establish tentative sizing criteria for V/STOL wind-tunnel testing with small wall effects. The report is one of the series 515-522 of papers presented at the 27th meeting of the AGARD Flight Mechanics Panel, held 11-12 October 1965 in Rome, Italy. (Author).
Aerodynamic Stability And Control Wind Tunnel Data Correlation
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Author : G. R. Casteel
language : en
Publisher:
Release Date : 1971
Aerodynamic Stability And Control Wind Tunnel Data Correlation written by G. R. Casteel and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1971 with Flight control categories.
The general objective was to collect and analyze aerodynamic stability and control data for the XV-4B, XV-5A, and P-1127 VTOL configurations. Correlation and analysis of existing model data were made to investigate hover and transition characteristics. Particular emphasis was placed on the aerodynamic power effects, sometimes referred to as interference effects. Other areas of investigation were sometimes referred to as interference effects. Other areas of investigation were nondimensional coefficients used to present VTOL data and wind tunnel test techniques. Wind tunnel tests were conducted using an inlet only model and a jet only model to investigate special test and analysis problems for these components. The agreement between different sets of XV-4B model data was, in general, found to be poor. However, the nondimensional coefficients used by Lockheed to reduce to XV-4B model data appear to be valid parameters for this category of VTOL airplane. The jet entrainment flow was shown by experiment to be the primary cause of the XV-4B power effects, and the XV-4B jet path was experimentally and theoretically determined.
Wind Tunnel Flight Correlation Study Of Aerodynamic Characteristics Of A Large Flexible Supersonic Cruise Airplane Xb 70 1 Extrapolation Of Wind Tunnel Data To Full Scale Conditions
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Author :
language : en
Publisher:
Release Date : 1980
Wind Tunnel Flight Correlation Study Of Aerodynamic Characteristics Of A Large Flexible Supersonic Cruise Airplane Xb 70 1 Extrapolation Of Wind Tunnel Data To Full Scale Conditions written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aerodynamics, Supersonic categories.
Wind Tunnel Flight Correlation Study Of Aerodynamic Characteristics Of A Large Flexible Supersonic Cruise Airplane Xb 70 1 A Comparison Between Characteristics Predicted From Wind Tunnel Measurements And Those Measured In Flight
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Author :
language : en
Publisher:
Release Date : 1980
Wind Tunnel Flight Correlation Study Of Aerodynamic Characteristics Of A Large Flexible Supersonic Cruise Airplane Xb 70 1 A Comparison Between Characteristics Predicted From Wind Tunnel Measurements And Those Measured In Flight written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1980 with Aerodynamics, Supersonic categories.
Scientific And Technical Aerospace Reports
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Author :
language : en
Publisher:
Release Date : 1994
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1994 with Aeronautics categories.