Wind Tunnel/flight Data Correlation for the Boeing 737-100 Transport Airplane PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Wind Tunnel/flight Data Correlation for the Boeing 737-100 Transport Airplane PDF full book. Access full book title Wind Tunnel/flight Data Correlation for the Boeing 737-100 Transport Airplane by Francis J. Capone. Download full books in PDF and EPUB format.
Author: Francis J. Capone Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 18
Book Description
"A brief wind-tunnel/flight data correlation for the Boeing 737-100 airplane has been made. The wind-tunnel data were published in NASA TN D-5971. The results showed excellent agreement between wind-tunnel and flight trimmed drag polars at Mach numbers less than 0.67. The _wind-tunnel data predicted larger drag increments due to compressibility and a lift-curve slope about 9 percent higher than flight."--Abstract.
Author: Francis J. Capone Publisher: ISBN: Category : Aerodynamics Languages : en Pages : 18
Book Description
"A brief wind-tunnel/flight data correlation for the Boeing 737-100 airplane has been made. The wind-tunnel data were published in NASA TN D-5971. The results showed excellent agreement between wind-tunnel and flight trimmed drag polars at Mach numbers less than 0.67. The _wind-tunnel data predicted larger drag increments due to compressibility and a lift-curve slope about 9 percent higher than flight."--Abstract.
Author: James A. Behal Publisher: ISBN: Category : Buffeting (Aerodynamics) Languages : en Pages : 506
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.
Author: James A. Behal Publisher: 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.
Author: James A. Behal Publisher: ISBN: Category : Buffeting (Aerodynamics) Languages : bo Pages : 1104
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.
Author: James A. Behal Publisher: ISBN: Category : Buffeting (Aerodynamics) Languages : en Pages : 656
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.
Author: Francis J. Capone
Author: Francis J. Capone
Author: James A. Behal
Author: James A. Behal
Author: 
Author: 
Author: 
Author: 
Author: James A. Behal
Author: James A. Behal
Author: Donald L. Loving