A Wind-tunnel Investigation to Evaluate the Aerodynamic Performance of Three Different Airplane Configurations Having Arrow- and Delta-wing Plan Forms at a Mach Number of 2.91

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Publisher :
ISBN 13 :
Total Pages : 109 pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis A Wind-tunnel Investigation to Evaluate the Aerodynamic Performance of Three Different Airplane Configurations Having Arrow- and Delta-wing Plan Forms at a Mach Number of 2.91 by : James N. Mueller

Download or read book A Wind-tunnel Investigation to Evaluate the Aerodynamic Performance of Three Different Airplane Configurations Having Arrow- and Delta-wing Plan Forms at a Mach Number of 2.91 written by James N. Mueller and published by . This book was released on 1959 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Wind-tunnel Investigation of the Aerodynamic Characteristics of Three Airplane Configurations Having Diamond-plan-form Wings at a Mach Number of 2.91

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Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis A Wind-tunnel Investigation of the Aerodynamic Characteristics of Three Airplane Configurations Having Diamond-plan-form Wings at a Mach Number of 2.91 by : John E. Grimaud

Download or read book A Wind-tunnel Investigation of the Aerodynamic Characteristics of Three Airplane Configurations Having Diamond-plan-form Wings at a Mach Number of 2.91 written by John E. Grimaud and published by . This book was released on 1960 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Introduction to Aircraft Flight Mechanics

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Publisher : AIAA
ISBN 13 : 9781600860782
Total Pages : 666 pages
Book Rating : 4.8/5 (67 download)

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Book Synopsis Introduction to Aircraft Flight Mechanics by : Thomas R. Yechout

Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

Wind-tunnel Investigation of Aerodynamic Efficiency of Three Planar Elliptical Wings with Curvature of Quarter-chord Line

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Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Wind-tunnel Investigation of Aerodynamic Efficiency of Three Planar Elliptical Wings with Curvature of Quarter-chord Line by : Raymond E. Mineck

Download or read book Wind-tunnel Investigation of Aerodynamic Efficiency of Three Planar Elliptical Wings with Curvature of Quarter-chord Line written by Raymond E. Mineck and published by . This book was released on 1993 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flight Stability and Automatic Control

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Publisher : WCB/McGraw-Hill
ISBN 13 : 9780071158381
Total Pages : 441 pages
Book Rating : 4.1/5 (583 download)

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Book Synopsis Flight Stability and Automatic Control by : Robert C. Nelson

Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.

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

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Publisher :
ISBN 13 :
Total Pages : 292 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 by : Richard J. Re

Download or read book Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92 written by Richard J. Re and published by . This book was released on 1993 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Apollo Wind Tunnel Testing Program

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Publisher :
ISBN 13 :
Total Pages : 84 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Apollo Wind Tunnel Testing Program by : William C. Moseley (Jr.)

Download or read book Apollo Wind Tunnel Testing Program written by William C. Moseley (Jr.) and published by . This book was released on 1966 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Investigation of Three-dimensional Wall Interference in a Variable Porosity Transonice Wind Tunnel

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Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis An Investigation of Three-dimensional Wall Interference in a Variable Porosity Transonice Wind Tunnel by : Travis W. Binion (Jr.)

Download or read book An Investigation of Three-dimensional Wall Interference in a Variable Porosity Transonice Wind Tunnel written by Travis W. Binion (Jr.) and published by . This book was released on 1974 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind Tunnel/flight Data Correlation (u).

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Publisher :
ISBN 13 :
Total Pages : 692 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Wind Tunnel/flight Data Correlation (u). by : James A. Behal

Download or read book Wind Tunnel/flight Data Correlation (u). written by James A. Behal and published by . This book was released on 1971 with total page 692 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Subsonic Wind-tunnel Investigation of the Aerodynamic Effects of Pivoting a Low-aspect-ratio Wing to Large Yaw Angles with Respect to the Fuselage to Increase Lift-drag Ratio

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Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Subsonic Wind-tunnel Investigation of the Aerodynamic Effects of Pivoting a Low-aspect-ratio Wing to Large Yaw Angles with Respect to the Fuselage to Increase Lift-drag Ratio by : Thomas G. Gainer

Download or read book Subsonic Wind-tunnel Investigation of the Aerodynamic Effects of Pivoting a Low-aspect-ratio Wing to Large Yaw Angles with Respect to the Fuselage to Increase Lift-drag Ratio written by Thomas G. Gainer and published by . This book was released on 1960 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind Tunnel Investigation of Vortex Flows on F/A-18 Configuration at Subsonic Through Transonic Speeds

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Publisher :
ISBN 13 :
Total Pages : 172 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Wind Tunnel Investigation of Vortex Flows on F/A-18 Configuration at Subsonic Through Transonic Speeds by : Gary E. Erickson

Download or read book Wind Tunnel Investigation of Vortex Flows on F/A-18 Configuration at Subsonic Through Transonic Speeds written by Gary E. Erickson and published by . This book was released on 1991 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Investigation of Aerodynamic Performance, Steady and Vibratory Loads, Surface Temperatures, and Acoustic Characteristics of a Large-scale Twin-engine Upper-surface Blown Jet-flap Configuration

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Publisher :
ISBN 13 :
Total Pages : 208 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Wind-tunnel Investigation of Aerodynamic Performance, Steady and Vibratory Loads, Surface Temperatures, and Acoustic Characteristics of a Large-scale Twin-engine Upper-surface Blown Jet-flap Configuration by :

Download or read book Wind-tunnel Investigation of Aerodynamic Performance, Steady and Vibratory Loads, Surface Temperatures, and Acoustic Characteristics of a Large-scale Twin-engine Upper-surface Blown Jet-flap Configuration written by and published by . This book was released on 1976 with total page 208 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Low-speed Wind Tunnel Investigation of the Aerodynamic Characteristics of an Airplane Having a Cambered Arrow Wing with a 75 Deg Swept Leading Edge

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ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Low-speed Wind Tunnel Investigation of the Aerodynamic Characteristics of an Airplane Having a Cambered Arrow Wing with a 75 Deg Swept Leading Edge by :

Download or read book Low-speed Wind Tunnel Investigation of the Aerodynamic Characteristics of an Airplane Having a Cambered Arrow Wing with a 75 Deg Swept Leading Edge written by and published by . This book was released on 1960 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Longitudinal Airplane Dynamics Wind Tunnel Test Equipment

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Publisher :
ISBN 13 :
Total Pages : 246 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Longitudinal Airplane Dynamics Wind Tunnel Test Equipment by : O. B. Tufts

Download or read book Longitudinal Airplane Dynamics Wind Tunnel Test Equipment written by O. B. Tufts and published by . This book was released on 1955 with total page 246 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Buffeting Measurements on Two Wing End-plate Airplane Model Configurations

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Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Wind-tunnel Buffeting Measurements on Two Wing End-plate Airplane Model Configurations by : William B. Igoe

Download or read book Wind-tunnel Buffeting Measurements on Two Wing End-plate Airplane Model Configurations written by William B. Igoe and published by . This book was released on 1967 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

CFD Wing/pylon/finned Store Mutual Interference Wind Tunnel Experiment

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Publisher :
ISBN 13 :
Total Pages : 74 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis CFD Wing/pylon/finned Store Mutual Interference Wind Tunnel Experiment by : E. Rolland Heim

Download or read book CFD Wing/pylon/finned Store Mutual Interference Wind Tunnel Experiment written by E. Rolland Heim and published by . This book was released on 1991 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Wind-tunnel Studies at Subsonic and Transonic Speeds of a Multiple-mission Variable-wing- Sweep Airplane Configuration

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Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Wind-tunnel Studies at Subsonic and Transonic Speeds of a Multiple-mission Variable-wing- Sweep Airplane Configuration by : William J. Alford

Download or read book Wind-tunnel Studies at Subsonic and Transonic Speeds of a Multiple-mission Variable-wing- Sweep Airplane Configuration written by William J. Alford and published by . This book was released on 1959 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: