National Advisory Committee for Aeronautics (NACA) - 485 Matching Results

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Primary view of An active particle diffusion theory of flame quenching for laminar flames
Simon, Dorothy M. & Belles, Frank E.
March 4, 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: 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 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 Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full-Span Flap Type of Control With Overhang Balance: Transonic-Bump Method
Lockwood, Vernard E. & Hagerman, John R.
January 25, 1952
Primary view of Aerodynamic characteristics at transonic speeds of a wing having a 45 degree sweep, aspect ratio 8, taper ratio 0.45, and airfoil sections varying from the NACA 63A010 section at the root to the NACA 63A006 section at the tip.
Morrison, William D., Jr. & Fournier, Paul G.
January 15, 1952
Primary view of The aerodynamic characteristics at transonic speeds of an all-movable, tapered, 45 degrees sweptback, aspect-ratio-4 tail surface deflected about a skewed hinge axis
Hammond, Alexander D. & Watson, James M.
July 3, 1952
Primary view of Aerodynamic characteristics extended to high angles of attack at transonic speeds of a small-scale 0 degree sweep wing, 45 degree sweptback wing, and 60 degree delta wing
Wiley, Harleth G.
November 18, 1952
Primary view of The aerodynamic characteristics of a supersonic aircraft configuration with a 40 degree sweptback wing through a Mach number range from 0 to 2.4 obtained from various sources
Spearman, M. Leroy & Robinson, Ross B.
April 11, 1952
Primary view of Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds
Boyd, John W.
July 22, 1952
Primary view of Aerodynamic Characteristics of Two Delta Wings at Mach Number 4.04 and Correlations of Lift and Minimum-Drag Data for Delta Wings at Mach Numbers From 1.62 to 6.9
Ulmann, Edward F. & Dunning, Robert W.
December 23, 1952
Primary view of Aerodynamic characteristics of two-plane, unswept tapered wings of aspect ratio 3 and 3-percent thickness from tests on a transonic bump
Emerson, Horace F. & Gale, Bernard M.
May 2, 1952
Primary view of Aerodynamic Load Measurements Over a Leading-Edge Slat on a 40 Degree Sweptback Wing at Mach Numbers From 0.10 to 0.91
Cahill, Jones F. & Nuber, Robert J.
September 23, 1952
Primary view of Aerodynamic Loading Characteristics of a Wing-Fuselage Combination Having a Wing of 45 Degrees Sweepback Measured in the Langley 8-Foot Transonic Tunnel
Loving, Donald L. & Williams, Claude V.
May 19, 1952
Primary view of Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 2: aerodynamic load distributions of series of five bodies having conical noses and cylindrical afterbodies
Jack, John R. & Gould, Lawrence I.
May 8, 1952
Primary view of Aeronautical Characteristics of a 45 Degree Sweptback Wing-Fuselage Combination and the Fuselage Alone Obtained in the Langley 8-Foot Transonic Tunnel
Osborne, Robert S. & Mugler, John P., Jr.
September 16, 1952
Primary view of Aeronautical interference effects on normal and axial force coefficients of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0
Kremzier, Emil J. & Dryer, Murray
April 28, 1952
Primary view of Altitude Investigation of Gas Temperature Distribution at Turbine of Three Similar Axial-Flow Turbojet Engines
Prince, W. R. & Schulze, F. W.
August 6, 1952
Primary view of Altitude investigation of three flame-holder and fuel-systems configurations in a short converging afterburner on a turbojet engine
Braithwaite, Willis M.; Renas, Paul E. & Jansen, Emmert T.
September 10, 1952
Primary view of Altitude operational characteristics of a prototype model of the J47D (RX1-1 and RX1-3) turbojet engines with integrated electronic control
Bloomer, Harry E.; Conrad, E. William & Sobolewski, Adam E.
January 8, 1952
Primary view of Altitude performance investigation of single- and double-annular turbojet-engine combustors with various size fuel nozzles
Harp, James L., Jr. & Vincent, Kenneth R.
June 9, 1952
Primary view of Altitude performance investigation of two flame-holder and fuel-system configurations in short afterburner
Huntley, S. C. & Wilsted, H. D.
May 6, 1952
Primary view of Altitude performance of annular combustor type turbojet engine with JFC-2 fuel
Useller, James W.; Harp, James L., Jr. & Barson, Zelmar
February 5, 1952
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