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Wind Tunnel Investigation At High Subsonic Speeds To Determine The Rolling Derivatives Of Two Wing Fuselage Combinations Having Triangular Winds Including A Semiempirical Method Of Estimating The Rolling Derivatives
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Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives by : James W. Wiggins
Download or read book Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives written by James W. Wiggins and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13 [degrees] and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives by : James W. Wiggins
Download or read book Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13 [degrees] and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives written by James W. Wiggins and published by . This book was released on 1958 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Measurements and Estimated Values of the Rolling Stability Derivatives of a Variable-sweep Airplane Configuration at Subsonic and Transonic Speeds by :
Download or read book Wind-tunnel Measurements and Estimated Values of the Rolling Stability Derivatives of a Variable-sweep Airplane Configuration at Subsonic and Transonic Speeds written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers by : Benjamin H. Beam
Download or read book A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers written by Benjamin H. Beam and published by . This book was released on 1955 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is described for measuring the dynamic stability derivatives of a model airplane in a wind tunnel. The characteristics features of this system are that single-degree-of-freedom oscillations were used to obtain combinations of rolling, yawing, and pitching motions; that the oscillations were excited and controlled by velocity feedback which permitted operation under conditions unfavorable for more conventional types of oscillatory testing; and that data processing was greatly simplified by using analog computer elements in the strain-gage circuitry.
Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds of the Static Longitudinal and Static Lateral Stability Characteristics of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 2.31 and an NACA 65A003 Airfoil by : James W. Wiggins
Download or read book Wind-tunnel Investigation at High Subsonic Speeds of the Static Longitudinal and Static Lateral Stability Characteristics of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 2.31 and an NACA 65A003 Airfoil written by James W. Wiggins and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings by : Willard G. Smith
Download or read book A Wind-tunnel Investigation at Subsonic and Low Supersonic Speeds of a Re-entry Vehicle with Retractable Wings written by Willard G. Smith and published by . This book was released on 1961 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail [with List of References] by :
Download or read book Wind-tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail [with List of References] written by and published by . This book was released on 1959 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wall Interference in Wind Tunnels with Slotted and Porous Boundaries at Subsonic Speeds by : Barrett Stone Baldwin
Download or read book Wall Interference in Wind Tunnels with Slotted and Porous Boundaries at Subsonic Speeds written by Barrett Stone Baldwin and published by . This book was released on 1953 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Linearized compressible-flow analysis is applied to the study of wind-tunnel-wall interference for subsonic flow in either two-dimensional or circular test sections having slotted or porous walls. Expressions are developed for evaluating blockage and lift interference.
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 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind Tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics by : Isidore G. Recant
Download or read book Wind Tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics written by Isidore G. Recant and published by . This book was released on 1942 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: Combinations of an NACA 23012 tapered wing and a circular fuselage having a wedge-shaped rear were tested in the NACA 7- by 10-foot wind tunnel to determine the effect of wing-fuselage interference on the lateral-stability of wing-fuselage interference on the lateral-stability characteristics. The model configurations represented a high-wing, a mid-wing, and a low-wing monoplane. For each configuration, tests were made with a partial-span split flap neutral and deflected 60 degrees and with and without a vertical tail. Tests of the fuselage alone and of the fuselage with the vertical tail were also made.
Book Synopsis Wind Tunnel Measurements at Subsonic and Transonic Speeds of the Rolling Stability Derivatives of a Variable Sweep Airplane Configuration Outer Wing Panels Swept 108 by : William C. Jr Hayes
Download or read book Wind Tunnel Measurements at Subsonic and Transonic Speeds of the Rolling Stability Derivatives of a Variable Sweep Airplane Configuration Outer Wing Panels Swept 108 written by William C. Jr Hayes and published by . This book was released on 1961 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation to Determine the Aerodynamic Characteristics in Steady Roll of a Model at High Subsonic Speeds by : Richard E. Kuhn
Download or read book Wind-tunnel Investigation to Determine the Aerodynamic Characteristics in Steady Roll of a Model at High Subsonic Speeds written by Richard E. Kuhn and published by . This book was released on 1953 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section by : Harold S. Johnson
Download or read book Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination with Quarter-chord Line Swept Back 32.6 Degrees and NACA 65A006 Airfoil Section written by Harold S. Johnson and published by . This book was released on 1953 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross-section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing by : Thomas J. Jr King
Download or read book Wind-tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross-section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characterisitcs of a Model Having a 45 Degree Swept Wing written by Thomas J. Jr King and published by . This book was released on 1956 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Approximation of the Spanwise Distribution of Wind-tunnel-boundary Interference on Lift of Wings in Rectangular Perforated-wall Test Sections by : Ray H. Wright
Download or read book Approximation of the Spanwise Distribution of Wind-tunnel-boundary Interference on Lift of Wings in Rectangular Perforated-wall Test Sections written by Ray H. Wright and published by . This book was released on 1968 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximation method has been developed for calculating the spanwise distribution of wind-tunnel-boundary upwash interference on lift of wings in rectangular perforated-wall test sections. This method is applied to square test sections with an assumed effective permeability constant of 0.6. A problem of considerable difficulty in practical application of the method presented is the estimation of an effective permeability constant. Because of the variation of the upwash interference with Mach number and of the influence of boundary layer on the effective permeability factor, the boundary interference in a perforated-wall wind-tunnel test section at high subsonic Mach numbers is likely to be of the nature of that in an open-throat tunnel.
Book Synopsis Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls by : Robert E. Dannenberg
Download or read book Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-speed Wind Tunnel as Affected by the Tunnel Walls written by Robert E. Dannenberg and published by . This book was released on 1950 with total page 678 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tunnel-wall corrections for the induced upwash velocity for a swept wing completely spanning a rectangular wind tunnel are included in the appendix.
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