Wind tunnel tests of five strut sections in yaw /

Wind tunnel tests of five strut sections in yaw /

Saved in:

Bibliographic Details
Main Author:	Warner, Edward Pearson, 1894-1958 (Author)
Format:	Government Document Electronic eBook
Language:	English
Published:	[Washington, D.C.] : National Advisory Committee for Aeronautics, 1923.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 167.
Subjects:	Yawing (Aerodynamics) Airplanes > Models. Struts (Engineering) Wind tunnel testing.
Online Access:	CONNECT

Similar Items

The estimation of the rate of change of yawing moment with sideslip /
by: Imlay, Frederick H.
Published: (1938)

Wind-tunnel investigation of effect of yaw on lateral-stability characteristics.
by: Bamber, M. J., et al.
Published: (1939)

Wind-tunnel investigation of effect of yaw on lateral-stability characteristics.
by: Bamber, M. J., et al.
Published: (1939)

Aerodynamic rolling and yawing moments produced by floating wing-tip ailerons, as measured by the spinning balance /
by: Bamber, Millard J.
Published: (1934)

Rolling, yawing, and hinge moments produced by rectangular ailerons (correlating Technical Reports nos. 298, 343, and 370) /
by: Heald, R. H.
Published: (1933)

Wind-tunnel investigation of the effect of vertical position of the wing on the side flow in the region of the vertical tail /
by: Recant, Isidore G., et al.
Published: (1941)

Effect of retractable-spoiler location on rolling- and yawing-moment coefficents /
by: Shortal, Joseph Adams, 1908-
Published: (1934)

Compressive strength of tapered airplane struts /
by: Lewe, Viktor
Published: (1923)

Wind-tunnel investigation of effect of yaw on lateral-stability characteristics.
by: Recant, Isidore G., et al.
Published: (1941)

The effect of slots and flaps on lateral control of a low-wing monoplane as determined in flight /
by: Soule, Hartley A. 1904-1988, et al.
Published: (1933)

Tests in the gust tunnel of a model of the XBM-1 airplane /
by: Donely, Philip, et al.
Published: (1939)

Wind-tunnel tests of the Fowler variable-area wing /
by: Weick, Fred E., et al.
Published: (1932)

Model supports and their effect on the results of wind tunnel tests /
by: Bacon, D. L.
Published: (1923)

Tests on built-up airplane struts having initial tension in outside fibers /
by: Schwamb, T. A., et al.
Published: (1923)

Spin tests of two models of a low-wing monoplane to investigate scale effect in the model test range /
by: Donlan, Charles J.
Published: (1941)

Method of correcting wind tunnel data for omitted parts of airplane models /
by: Smith, Richard Harbert, 1894-
Published: (1927)

Wind tunnel tests of fuselages and windshields /
by: Warner, Edward Pearson, 1894-1958
Published: (1925)

Analysis of a spin and recovery from time histories of attitudes and velocities as determined for a dynamic model of a contemporary fighter airplane in the free-spinning tunnel /
by: Scher, Stanley H.
Published: (1956)

The estimation of airplane performance from wind tunnel tests on conventional airplane models /
by: Warner, Edward Pearson, 1894-1958, et al.
Published: (1925)

The theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance /
by: Imlay, Frederick H.
Published: (1941)

Fuselage-drag tests in the variable-density wind tunnel : streamline bodies of revolution, fineness ratio of 5 /
by: Abbott, Ira H. A.
Published: (1937)

Wind-tunnel tests of a Hall high-lift wing /
by: Weick, Fred E., et al.
Published: (1932)

Wind tunnel pressure distribution tests on an airfoil with trailing edge flap /
by: Wenzinger, Carl J. 1903-1988, et al.
Published: (1929)

The effect of wind tunnel turbulence upon the forces measured on models /
by: LePage, Wynn Laurence, 1902-1985, et al.
Published: (1924)

Horizontal buoyancy in wind tunnels /
by: Zahm, Albert Francis, 1862-
Published: (1920)

The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel /
by: Stone, Ralph W., et al.
Published: (1950)

Wind-tunnel measurements of air loads on split flaps /
by: Wenzinger, Carl J. 1903-1988
Published: (1934)

Interference of wing and fuselage from tests of 17 combinations in the N.A.C.A. variable-density tunnel combinations with special junctures /
by: Sherman, Albert
Published: (1938)

Tests on a model of the D airplane T 39 of the "Deutsche Flugzeug Werke" (German Airplane Works) /
by: Molthan, Wilhelm
Published: (1924)

Calculations for a single-strut biplane with reference to the tensions in the wing bracing /
by: Blumenthal, Otto, 1876-1944
Published: (1923)

Wind tunnel pressure distribution tests on a series of biplane wing models.
by: Knight, Montgomery, et al.
Published: (1929)

Wind-tunnel tests of a Clark Y wing having split flaps with gaps /
by: Wenzinger, Carl J. 1903-1988
Published: (1938)

Wind tunnel force tests in wing systems through large angles of attack /
by: Wenzinger, Carl J. 1903-1988, et al.
Published: (1928)

Interference of wing and fuselage from tests of eight combinations in the N.A.C.A. variable-density tunnel combinations with tapered fillets and straight-side junctures /
by: Sherman, Albert
Published: (1938)

The effect of wing tip floating ailerons on the autorotation of a monoplane wing model /
by: Knight, Montgomery, et al.
Published: (1930)

The effects of some common surface irregularities on wing drag /
by: Hood, Manley J.
Published: (1939)

The reduction in drag of a forward-sloping windshield /
by: Jacobs, Eastman N. 1902-
Published: (1933)

The drag of a J-5 radial air-cooled engine /
by: Weick, Fred E.
Published: (1928)

Effect of the surface condition of a wing on the aerodynamic characteristics of an airplane /
by: DeFrance, Smith J.
Published: (1934)

The effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests /
by: Weick, Fred E., et al.
Published: (1929)