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Primary view of Aerodynamic Characteristics at High and Low Subsonic Mach Numbers of the NACA 0012, 64₂-015, and 64₃-018 Airfoil Sections at Angles of Attack from -2 Degrees to 30 Degrees
Critzos, Chris C.
July 23, 1954
Primary view of Aerodynamic characteristics at high speeds of a two-blade NACA 10-(3)(062)-045 propeller and of a two-blade NACA 10-(3)(08)-045 propeller
Solomon, William
October 1, 1948
Primary view of Aerodynamic characteristics at high speeds of full-scale propellers having Clark Y blade sections
Johnson, Peter J.
October 26, 1948
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.
May 6, 1948
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 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 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 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
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