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Wind Tunnel Investigation Of Effect Of Yaw On Lateral Stability Characteristics
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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 Investigation of Effect of Yaw on Lateral-stability Characteristics by : Millard J. Bamber
Download or read book Wind-tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics written by Millard J. Bamber and published by . This book was released on 1939 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: Four N.A.C.A. 23012 wings were tested at several angles in the N.A.C.A. 7- by 10-foot wind tunnel. All the wings have rounded tips and, in plan form, one is rectangular and the others are tapered 3:1 with various amounts of sweep. Each wing was tested with two amounts of dihedral and with partial-span split flaps.
Book Synopsis Wind Tunnel Investigation of Effect of Yaw on Lateral Stability Characteristics by : Millard J. Bamber
Download or read book Wind Tunnel Investigation of Effect of Yaw on Lateral Stability Characteristics written by Millard J. Bamber and published by . This book was released on 1939 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics by : Millard J. Bamber
Download or read book Wind-tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics written by Millard J. Bamber and published by . This book was released on 1939 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: An N.A.C.A. 23012 rectangular wing with rounded tips was tested in combination with a fuselage of circular cross section at several angles of yaw in the N.A.C.A. 7- by 10-foot wind tunnel. The model was tested as a high-wing, a midwing, and a low-wing monoplane; for each wing location, tests were made with two amounts of dihedral and with partial-span split flaps. For each combination of wing and fuselage, tests were made with and without a fin. Sample charts of the coefficients of rolling moment, yawing moment, and lateral force are given for some of the combinations tested. THe rate of change in the coefficients with angle of yaw is given for stability calculation.
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 1941 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel of Effect of Yaw on Lateral-stability Characteristics by : Isidore G. Recant
Download or read book Wind-tunnel of Effect of Yaw on Lateral-stability Characteristics written by Isidore G. Recant and published by . This book was released on 1941 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt: Model combinations of an NACA 23012 tapered wing and a circular fuselage were tested in the NACA 7- by 10-foot wind tunnel to determine the effect of longitudinal wing position on the change in lateral stability due to interference. The aerodynamic center of the wing was located at approximately 80, 130, and 180 percent of the mean locations, the model was tested as a high-wing, a mid-wing, and a low-wing monoplane. For each conbination, testes were made with a partial-span split flap neutral and deflected 60 degrees and with and without a vertical tail. The rearmost low-wing combination was tested with and without a fillet.
Book Synopsis Wind-tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics by : Arthur R. Wallace
Download or read book Wind-tunnel Investigation of Effect of Yaw on Lateral-stability Characteristics written by Arthur R. Wallace and published by . This book was released on 1943 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were made in the LMAL 7- by 10-foot tunnel to determine the effect of a horizontal tail on the lateral stability characteristics of a high-wing, a mid-wing, and a low-wing monoplane. The model combinations consisted of a circular fuselage, an NACA 23012 tapered wing, and an NACA 0009 horizontal tail surface. Each wing-fuselage combination was tested with a partial-span split flap neutral and deflected 60 degrees and with and without a single vertical tail. Tests were also made of the fuselage with and without the tail surfaces.
Book Synopsis Wind-tunnel Investigation of Effects of Tail Length on the Longitudinal and Lateral Stability Characteristics of a Single-propeller Airplane Model by : Harold S. Johnson
Download or read book Wind-tunnel Investigation of Effects of Tail Length on the Longitudinal and Lateral Stability Characteristics of a Single-propeller Airplane Model written by Harold S. Johnson and published by . This book was released on 1948 with total page 109 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented are lift, drag, and pitching-moment data, neutral points, and the effects of power, flap deflection, and free elevator for the model at zero angle of yaw. The lateral-stability parameters and tests for a yaw range including rudder-free data are also presented.
Book Synopsis Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg by :
Download or read book Low-speed Wind Tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 60 Deg written by and published by . This book was released on 1995 with total page 174 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 Deg by :
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 50 Deg written by and published by . This book was released on 1995 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models by : Isidore G. Recant
Download or read book Determination of the Stability and Control Characteristics of Airplanes from Tests of Powered Models written by Isidore G. Recant and published by . This book was released on 1942 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt: A technique of testing wind-tunnel powered models has been developed as a result of experience gained in the investigation of the static longitudinal and lateral stability and control characteristics of several powered models in the NACA 7- by 10-foot wind tunnel. As an important part of this technique, a minimum program of the tests considered necessary to specify satisfactorily the static stability and control characteristics for present-day airplanes has been tentatively established.
Book Synopsis Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Deg by :
Download or read book Low-speed Wind-tunnel Investigation of the Stability and Control Characteristics of a Series of Flying Wings with Sweep Angles of 70 Deg written by and published by . This book was released on 1995 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces by : Arthur Earl Bryson
Download or read book Experimental Determination of the Effect of Horizontal-tail Size, Tail Length, and Vertical Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45 ̊sweptback Wing and Tail Surfaces written by Arthur Earl Bryson and published by . This book was released on 1952 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation of the Flight Characteristics of a Canard General-aviation Airplane Configuration by : Dale R. Satran
Download or read book Wind-tunnel Investigation of the Flight Characteristics of a Canard General-aviation Airplane Configuration written by Dale R. Satran and published by . This book was released on 1986 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Langley Full-scale Tunnel Investigation of the Factors Affecting the Directional Stability and Trim Characteristics of a Fighter-type Airplane by : Harold H. Sweberg
Download or read book Langley Full-scale Tunnel Investigation of the Factors Affecting the Directional Stability and Trim Characteristics of a Fighter-type Airplane written by Harold H. Sweberg and published by . This book was released on 1945 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: Tests were made in the Langley full-scale tunnel of the Grumman XF6F-4 airplane in order to investigate the factors that affect the directional stability and trim characteristics of a typical fighter-type airplane. Eight representative flight conditions were investigated in detail. The separate contributions of the wing-fuselage combination, the vertical tail, and the propeller to the directional stability of the airplane in each condition were determined. Extensive air-flow surveys of sidewash angle and dynamic-pressure ratio along a line coincident with the rudder hinge line were made for each condition investigated to aid in evaluating the slipstream effects. The data obtained from the air-flow surveys were also used to investigate methods for calculating the contribution of the vertical tail to the airplane directional stability. The results of the tests showed that, for the conditions investigated, the directional stability of the airplane was smallest for the gliding condition with flaps retracted and was greatest for the wave-off condition with flaps deflected 50°. The variation of sidewash angle at the vertical tail with angle of yaw was destabilizing for all conditions investigated. Propeller operation increased the magnitude of the destabilizing sidewash but, at small angles of yaw, also increased the dynamic pressure at the vertical tail sufficiently to make the combined effect stabilizing.
Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 654 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90° by : John E. Grimaud
Download or read book Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack Up to 90° written by John E. Grimaud and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
