Technical Report Archive and Image Library (TRAIL) - Browse

ABOUT BROWSE FEED
Primary view of Additional experiments with flat-top wing- body combinations at high supersonic speeds
Gloria, H. R.; Syvertson, C. A. & Wong, T. J.
February 19, 1957
Primary view of Additional fatigue tests on effects of design details in 355-T6 sand-cast aluminum alloy
Eaton, I D & Youra, John A
March 10, 1954
Primary view of Additional free-flight tests of the rolling effectiveness of several wing-spoiler arrangements at high subsonic, transonic, and supersonic speeds
Strass, H Kurt
November 24, 1948
Primary view of Additional measurements of the low-speed static stability of a configuration employing three triangular wing panels and a body of equal length
Delany, Noel K
July 25, 1955
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 thickne
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.
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
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