National Advisory Committee for Aeronautics (NACA) - 5,164 Matching Results

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Primary view of Aerodynamic and hydrodynamic characteristics of a deck-inlet multijet water-based-aircraft configuration designed for supersonic flight
Bielat, Ralph P; Coffee, Claude W , Jr & Petynia, William W
December 5, 1956
Primary view of Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hydro-ski aircraft with a variable-incidence wing
Petynia, William W.; Hasson, Dennis F. & Spooner, Stanley H.
October 23, 1957
Primary view of Aerodynamic and hydrodynamic characteristics of models of some aircraft-towed mine-sweeping devices : TED No. NACA AR 8201
Shanks, Robert E.
December 1, 1955
Primary view of Aerodynamic and inlet-flow-field characteristics at a free-stream Mach number of 3.0 for airplanes with circular fuselage cross sections and for two engine locations
Dryer, Murray & Luidens, Roger W
March 18, 1958
Primary view of Aerodynamic and lateral-control characteristics of a 1/28-scale model of the Bell X-1 airplane wing-fuselage combination : transonic-bump method
Lockwood, Vernard E
May 5, 1950
Primary view of Aerodynamic characteristics and pressure distributions of a 6-percent-thick 49 degree sweptback wing with blowing over half-span and full-span flaps
Whittle, Edward F , Jr & Mclemore, H Clyde
September 20, 1955
Primary view of Aerodynamic characteristics at a Mach number of 1.25 of a 6-percent-thick triangular wing and 6- and 9-percent-thick triangular wings in combination with a fuselage : wing aspect ratio 2.31, biconvex airfoil sections
Hall, Albert W & Morris, Garland J
May 5, 1950
Primary view of Aerodynamic characteristics at a Mach number of 1.38 of four wings of aspect ratio 4 having quarter-chord sweep angles of 0 degrees, 35 degrees, 45 degrees, and 60 degrees
Kemp, William B , Jr; Goodson, Kenneth W & Booth, Robert A
October 10, 1950
Primary view of Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One with Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One with a Flared Afterbody and All-Movable Controls
Bernot, P. T. & Robinson, R. B.
August 4, 1958
Primary view of Aerodynamic characteristics at a Mach number of 6.8 of two hypersonic missile configurations, one with low-aspect-ratio cruciform fins and trailing-edge flaps and one with a flared afterbody and all-movable controls
Robinson, Ross B & Bernot, Peter T
August 4, 1958
Primary view of Aerodynamic characteristics at high and low subsonic Mach numbers of four NACA 6-series airfoil sections at angles of attack from -2 to 31 degrees
Wilson, Homer B., Jr. & Horton, Elmer A.
June 5, 1953
Primary view of Aerodynamic Characteristics at High and Low Subsonic Mach Numbers of the NACA 0012, 64(sub 2)-015, and 64(sub 3)-018 Airfoil Sections at Angles of Attack from -2 Degrees to 30 Degrees
Critzos, Chris C.
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 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 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