National Advisory Committee for Aeronautics (NACA) - Browse

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Primary view of Aerodynamic Characteristics at High Speeds of Full-Scale Propellers having Different Shank Designs
Maynard, Julian D.
February 13, 1947
Primary view of Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers
Maynard, Julian D & Salters, Leland B , Jr
1957?
Primary view of Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap
Dunning, Robert W & Ulmann, Edward F
May 29, 1953
Primary view of Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls
Spearman, M. Leroy & Robinson, Ross B.
August 30, 1954
Primary view of Aerodynamic characteristics at Mach number of 4.06 of a typical supersonic airplane model using body and vertical-tail wedges to improve directional stability
Dunning, Robert W
December 3, 1957
Primary view of Aerodynamic characteristics at Mach numbers 2.36 and 2.87 of an airplane configuration having a cambered arrow wing with a 75 degree swept leading edge
Hallissy, Joseph M , Jr & Hasson, Dennis F
August 4, 1958
Primary view of Aerodynamic characteristics at Mach numbers from 0.7 to 1.75 of a four-engine swept-wing airplane configuration as obtained from a rocket-propelled model test
Chapman, Rowe, Jr
September 2, 1955
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 R; 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 Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
Smith, Hamilton A & Schaefer, Raymond F
April 1950
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 I : 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 II : 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
Lockwood, Vernard E; Vogler, Raymond D & Turner, Thomas R
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
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
Driver, Cornelius & Robinson, Ross B
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 characteris
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