National Advisory Committee for Aeronautics (NACA) - 13,806 Matching Results

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Primary view of 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
Wiggins, James W.
August 28, 1953
Primary view of Wind-tunnel investigation at low and transonic speeds of the feasibility of self-actuating spoilers as a lateral-control device for a missile
Wiley, Harleth G. & Hayes, William C., Jr.
January 28, 1954
Primary view of Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of aspect ratio 1.59 equipped with various 25-percent chord plain flaps
Johnson, Harold S & Hageman, John R
August 1, 1950
Primary view of Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip
Blackaby, James R.
April 7, 1955
Primary view of Wind-tunnel investigation at low speed of a wing swept-back 63 degrees and twisted and cambered for a uniform load at a lift coefficient of 0.5
Weiberg, James A. & Carel, Hubert C.
May 9, 1950
Primary view of Wind-tunnel investigation at low speed of a wing swept back 63 degrees and twisted and cambered for uniform load at a lift coefficient of 0.5 and with a thickened tip section
Weiberg, James A. & Carel, Hubert C.
November 21, 1950
Primary view of Wind Tunnel Investigation at Low Speed of Aerodynamic Characteristics of Army Chemical Corps Model E-112 Bomblets with Span Chord Ratio of 2 - 1
Letko, W.
December 26, 1956
Primary view of Wind-tunnel investigation at low speed of an unswept untapered semispan wing of aspect ratio 3.13 equipped with various 25-percent-chord plain flaps
Johnson, Harold S & Hagerman, John R
April 1, 1950
Primary view of Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6
Jaquet, Byron M & Williams, James L
September 1, 1955
Primary view of Wind-tunnel investigation at low speed of effects of sideslip on static longitudinal trim and static lateral stability characteristics of three fighter-type airplane models
Jaquet, Byron M & Fletcher, H S
September 11, 1956
Primary view of Wind-tunnel investigation at low speed of sideslipping, rolling, yawing, and pitching characteristics for a model of a 45 degree swept-wing fighter-type airplane
Jaquet, Byron M & Fletcher, H S
September 1, 1955
Primary view of Wind-tunnel investigation at low speed of static and yawing characteristics of a 0.085-scale model of the Chance Vought XF8U-1 airplane : TED No. NACA DE 392
Jaquet, Byron M & Williams, James L
January 19, 1954
Primary view of Wind-tunnel investigation at low speed of the aerodynamic characteristics of the Army Chemical Corps model E112 bomblets
Letko, William & Williams, James L
November 4, 1955
Primary view of Wind tunnel investigation at low speed of the aerodynamic characteristics of the Army Chemical Corps model E112 bomblets
Letko, William & Williams, James L.
November 4, 1955
Primary view of Wind-tunnel investigation at low speed of the effects of chordwise wing fences and horizontal-tail position on the static longitudinal stability characteristics of an airplane model with a 35 degree sweptback wing
Queijo, M J; Jaquet, Byron M & Wolhart, Walter D
January 1, 1954
Primary view of Wind-tunnel investigation at low speed of the effects of symmetrical deflection of half-delta tip controls on the damping in roll and yawing moment due to rolling of a triangular-wing model
Wolhart, Water D
April 6, 1951
Primary view of Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model
Schneiter, Leslie E & Naeseth, Rodger L
November 1, 1948
Primary view of Wind-tunnel investigation at low speed of the lateral control characteristics of an unswept untapered semi-span wing of aspect ratio 3.13 equipped with various 25-percent-chord plain ailerons
Johnson, Harold S & Hagerman, John R
October 1, 1950
Primary view of Wind-Tunnel Investigation at Low Speed of the Pitching Stability Derivatives of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane, TED No. NACA DE 373
Queijo, M. J.; Wolhart, Walter D. & Fletcher, H. S.
July 13, 1953
Primary view of Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane, TED No. NACA DE 373
Queijo, M. J.; Wolhart, Walter D. & Fletcher, H. S.
May 20, 1953
Primary view of Wind-tunnel investigation at low speed of the rolling stability derivatives of a 1/10-scale model of the Douglas A4D-1 airplane
Wolhart, Walter D. & Fletcher, H. S.
October 7, 1954
Primary view of Wind-tunnel investigation at low speed of the rolling stability derivatives of a 1/10-scale model of the Douglas A4D-1 airplane : TED No. NACA DE 389
Wolhart, Walter D & Fletcher, H S
October 7, 1954
Primary view of Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/10-Scale Model of the Grumman F9F-9 Airplane, TED No. NACA AD 3109
Wolhart, Walter D. & Thomas, David F., Jr.
April 18, 1955
Primary view of Wind-Tunnel Investigation at Low Speed of the Static Longitudinal and Lateral Stability Characteristics of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane
Queijo, M. J.; Wolhart, W. D. & Fletcher, H. S.
February 11, 1953