National Advisory Committee for Aeronautics (NACA) - 5,157 Matching Results

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Primary view of Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight
Carmel, Melvin M.; Kelly, Thomas C. & Gregory, Donald T.
September 10, 1958
Primary view of Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 of Various Tip Controls on the Wing Panel of a 0.05-Scale Model of a Martin XASM-N-7 (Bullpup) Missile: TED No. NACA AD 3106
Driver, Cornelius
1956~
Primary view of Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness
Eggers, A. J., Jr.
November 6, 1947
Primary view of Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 1: maximum thickness at 20 percent of the chord
Berggren, Robert E. & Summers, James L.
November 19, 1948
Primary view of Aerodynamic characteristics at subsonic and supersonic Mach numbers of a thin triangular wing of aspect ratio 2 2: maximum thickness at midchord
Walker, Harold J. & Berggren, Robert E.
December 3, 1948
Primary view of Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness
Turner, Thomas R.; Lockwood, Vernard E. & Vogler, Raymond D.
January 12, 1949
Primary view of Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-Body Combinations Having Cambered Wings With an Aspect Ratio of 3.5 and a Taper Ratio of 0.2: Effect at M = 2.01 of Nacelle Shape and Position on the Aerodynamic Characteristics in Pitch of Two Wing-Body Combinations with 47 Degree Sweptback Wings
Driver, Cornelius
July 25, 1952
Primary view of Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2: Effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch
Robinson, Ross B. & Driver, Cornelius
January 10, 1952
Primary view of Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2: Effects of sweep angle and thickness ratio on the static lateral stability characteristics at M = 2.01
Hamilton, Clyde V.
August 1, 1952
Primary view of Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a 52.5 degree delta wing and a low, swept horizontal tail
Kehlet, Alan B.
March 29, 1954
Primary view of Aerodynamic characteristics at transonic speeds of a 60 degree delta wing equipped with a constant-chord flap-type control with and without an unshielded horn balance: transonic-bump method
Wiley, Harleth G. & Zontek, Leon
September 16, 1952
Primary view of Aerodynamic characteristics at transonic speeds of a 69 degree delta wing with a triangular plan-form control having a skewed hinge axis and an overhang balance: transonic-bump method
Wiley, Harleth G.
February 6, 1951
Primary view of The aerodynamic characteristics at transonic speeds of a model with a 45 degree sweptback wing, including the effect of leading edge slats and a low horizontal tail
Runckel, Jack F. & Schmeer, James W.
April 5, 1954
Primary view of Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full-Span Flap Type of Control With Overhang Balance: Transonic-Bump Method
Lockwood, Vernard E. & Hagerman, John R.
January 25, 1952
Primary view of Aerodynamic characteristics at transonic speeds of a wing having a 45 degree sweep, aspect ratio 8, taper ratio 0.45, and airfoil sections varying from the NACA 63A010 section at the root to the NACA 63A006 section at the tip.
Morrison, William D., Jr. & Fournier, Paul G.
January 15, 1952
Primary view of The Aerodynamic Characteristics at Transonic Speeds of an All-Movable, Tapered, 45 Degree Sweptback, Aspect-Ratio-4 Tail Deflected About a Skewed Hinge Axis and Equipped with an Inset Unbalancing Tab
Watson, James M.
September 29, 1953
Primary view of The aerodynamic characteristics at transonic speeds of an all-movable, tapered, 45 degrees sweptback, aspect-ratio-4 tail surface deflected about a skewed hinge axis
Hammond, Alexander D. & Watson, James M.
July 3, 1952
Primary view of Aerodynamic characteristics extended to high angles of attack at transonic speeds of a small-scale 0 degree sweep wing, 45 degree sweptback wing, and 60 degree delta wing
Wiley, Harleth G.
November 18, 1952
Primary view of Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a 1/14-Scale Model of the Grumman XF104 Airplane with Wing Sweepback of 42.5 Degrees
Kuhn, Richard E. & Draper, John W.
August 18, 1953
Primary view of The Aerodynamic Characteristics in Pitch of a 1/15-Scale Model of the Grumman F11F-1 Airplane at Mach Numbers of 1.41, 1.61, and 2.01, TED No. NACA DE 390
Driver, Cornelius
May 23, 1956
Primary view of Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01
Spearman, M. Leroy
October 30, 1953
Primary view of Aerodynamic characteristics including effects of wing fixes of a 1/20-scale model of the Convair F-102 airplane at transonic speeds
Osborne, Robert S. & Wornom, Dewey E.
March 18, 1954
Primary view of Aerodynamic characteristics including pressure distribution of a fuselage and three combinations of the fuselage with swept-back wings at high subsonic speeds
Sutton, Fred B. & Martin, Andrew
February 6, 1951
Primary view of Aerodynamic Characteristics Including Scale Effect of Several Wings and Bodies Alone and in Combination at a Mach Number of 1.53
Van Dyke, Milton D.
December 20, 1946
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