National Advisory Committee for Aeronautics (NACA) - Browse

ABOUT BROWSE FEED
Primary view of Aero dopes and varnishes
Britton, H T S
July 1927
Primary view of An aerodynamic analysis of the autogiro rotor with a comparison between calculated and experimental results
Wheatley, John B
1934
Primary view of The aerodynamic analysis of the gyroplane rotating-wing system
Wheatley, John B
March 1934
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 hydrodynamic tests of a family of models of flying-boat hulls derived from a streamline body : NACA model 84 series
Luoma, Arvo A
September 1943
Primary view of Aerodynamic and hydrodynamic tests of a family of models of flying hulls derived from a streamline body -- NACA model 84 series
Parkinson, John B; Olson, Roland E; Draley, Eugene C & Luoma, Arvo A
1943?
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 The aerodynamic aspect of wing-fuselage fillets
Muttray, H
February 1935
Primary view of The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
Chang, Chieh-Chien
October 1951
Primary view of Aerodynamic characteristics and flap loads of perforated double split flaps on a rectangular NACA 23012 airfoil
Turner, Thomas R
January 1943
Primary view of Aerodynamic characteristics and flap loads of the brake-flap installation on the 0.40-scale model of the F4F-3 left wing panel
Liddell, Robert B
October 1942
Primary view of Aerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and supersonic speeds
Mitcham, Grady L; Stevens, Joseph E & Norris, Harry P
November 1956
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