Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static-Stability and Control Characteristics of a 0.03-Scale Model of an Interim Development Version of the B-70 Airplane PDF Download

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Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static-Stability and Control Characteristics of a 0.03-Scale Model of an Interim Development Version of the B-70 Airplane

Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static-Stability and Control Characteristics of a 0.03-Scale Model of an Interim Development Version of the B-70 Airplane PDF Author: James C. Daugherty
Publisher:
ISBN:
Category :
Languages : en
Pages : 310

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Book Description

Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static-Stability and Control Characteristics of a 0.03-Scale Model of an Interim Development Version of the B-70 Airplane

Wind Tunnel Investigation at Supersonic Speeds of the Lift, Drag, Static-Stability and Control Characteristics of a 0.03-Scale Model of an Interim Development Version of the B-70 Airplane PDF Author: James C. Daugherty
Publisher:
ISBN:
Category :
Languages : en
Pages : 310

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Book Description

Wind-tunnel Investigation at Mach Numbers from 0.8 to 1.4 of Static Longitudinal and Lateral-directional Characteristics of an Unswept-wing Airplane Model

Wind-tunnel Investigation at Mach Numbers from 0.8 to 1.4 of Static Longitudinal and Lateral-directional Characteristics of an Unswept-wing Airplane Model PDF Author: James L. Summers
Publisher:
ISBN:
Category :
Languages : en
Pages : 99

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Book Description

Longitudinal Airplane Dynamics Wind Tunnel Test Equipment

Longitudinal Airplane Dynamics Wind Tunnel Test Equipment PDF Author: O. B. Tufts
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 246

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Book Description

Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92

Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 292

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Book Description

Wind-tunnel Investigation at Mach Numbers from 1.60 to 4.50 of Static Stability Characteristics of 2 Nonlifting Vehicles Suitable for Reentry

Wind-tunnel Investigation at Mach Numbers from 1.60 to 4.50 of Static Stability Characteristics of 2 Nonlifting Vehicles Suitable for Reentry PDF Author:
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 34

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Book Description

A Wind Tunnel Investigation of the Static Stability, Dynamic Stability, and Aerodynamic Performance of the SUNYAB Ultralight Aircraft

A Wind Tunnel Investigation of the Static Stability, Dynamic Stability, and Aerodynamic Performance of the SUNYAB Ultralight Aircraft PDF Author: Mark James Zima
Publisher:
ISBN:
Category :
Languages : en
Pages : 286

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Book Description

Wind Tunnel/flight Data Correlation (u).

Wind Tunnel/flight Data Correlation (u). PDF Author: James A. Behal
Publisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 692

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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 Investigation of the Longitudinal Dynamic Stability of a Model Airplane

Wind Tunnel Investigation of the Longitudinal Dynamic Stability of a Model Airplane PDF Author: Percy Hugh Francis Miller
Publisher:
ISBN:
Category :
Languages : en
Pages : 82

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Book Description

Wind Tunnel Investigation of an All Flush Orifice Air Data System for a Large Subsonic Aircraft

Wind Tunnel Investigation of an All Flush Orifice Air Data System for a Large Subsonic Aircraft PDF Author: Terry J. Larson
Publisher:
ISBN:
Category : Air speed
Languages : en
Pages : 104

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Book Description

Wind Tunnel Measurement of Static Stability and Control Characteristics of a Representative Supersonic Interceptor Airplane at Mach Numbers from 0.8 to 1.2

Wind Tunnel Measurement of Static Stability and Control Characteristics of a Representative Supersonic Interceptor Airplane at Mach Numbers from 0.8 to 1.2 PDF Author: Dana S. Morse
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 120

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Book Description