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Primary view of Additional Results in a Free-Flight Investigation of Control Effectiveness of Full-Span, 0.2-Chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Aspect Ratio, Taper, and Section Thickness Ratio
Sandahl, Carl A. & Strass, H. Kurt
April 23, 1948
Primary view of Additional results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a series of related afterbodies
Henry, Beverly Z., Jr. & Cahn, Maurice S.
September 24, 1956
Primary view of Additional Results on the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds
Spreeman, Kenneth P. & Few, Albert G., Jr.
August 10, 1954
Primary view of Additional Studies of the Stability and Controllability of an Unswept-Wing Vertically Rising Airplane Model in Hovering Flight Including Studies of Various Tethered Landing Techniques
Bates, William R.; Lovell, Powell M., Jr. & Smith, Charles C., Jr.
November 6, 1951
Primary view of The adhesion of molten boron oxide to various materials
Witzke, W. R.
April 1, 1958
Primary view of Adhesive and protective characteristics of ceramic coating A-417 and its effect on engine life of forged Refractaloy-26 (AMS 5760) and cast stellite 21 (AMS 5385) turbine blades
Garrett, Floyd B. & Gyorgak, Charles A.
February 12, 1953
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
Robinson, Ross B. & Bernot, Peter T.
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, 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 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
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