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Primary view of Acceleration Measurements During Landing in Rough Water of a 1/7-Scale Dynamic Model of Grumman XJR2F-1 Amphibian - Langley Tank Model 212: TED No. NACA 2378
Land, Norman S. & Zeck, Howard
May 6, 1947
Primary view of An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Gerus, Theodore F.; Powers, Albert G. & Heppler, Herbert J.
May 12, 1958
Primary view of An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Gerus, Theodore F.; Powers, Albert G. & Heppler, Herbert J.
May 12, 1958
Primary view of Adaptation of Combustion Principles to Aircraft Propulsion Volume 2: Combustion in Air-Breathing Jet Engines
Fuels and Combustion Research Division
May 2, 1956
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 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 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 The Aerodynamic Characteristics in Pitch of a 1/15-Scale Model of the Grumman F11F-1 Airplane at Mach Numbers of 1.41, 1.61, and 2.01, TED No. NACA DE 390
Driver, Cornelius
May 23, 1956
Primary view of Aerodynamic Characteristics of a 42 Degree Swept-Back Wing With Aspect Ratio 4 and NACA 64(Sub 1)-112 Airfoil Sections at Reynolds Numbers From 1,700,000 to 9,500,000
Neely, Robert H. & Conner, D. William
May 23, 1947
Primary view of Aerodynamic Characteristics of a Portion of the Horizontal Tail from a Douglas C-74 Airplane with Fabric-Covered Elevators
Perone, Angelo & Berthold, Cecil L.
May 6, 1947
Primary view of Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A004 airfoil section: Transonic-bump method
Myers, Boyd C., II & Wiggins, James W.
May 8, 1950
Primary view of Aerodynamic Characteristics of Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-Stream Mach Numbers From 1.50 to 1.99
Cohen, Robert J.
May 22, 1951
Primary view of Aerodynamic Characteristics of Several NACA Airfoil Sections at Seven Reynolds Numbers From 0.7 X 10(Exp 6) to 9.0 X 10(Exp 6)
Loftin, Laurence K., Jr. & Poteat, M. Irene
May 27, 1948
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 The Aerodynamic Characteristics of Two Series of Lifting Bodies at Mach Number 6.86
Ridyard, Herbert W.
May 24, 1954
Primary view of Aerodynamic characteristics of various configurations of a model of a 45 degree swept-wing airplane at a Mach number of 2.01
Spearman, M. Leroy; Driver, Cornelius & Robinson, Ross B.
May 26, 1955
Primary view of Aerodynamic Characteristics of Wings Designed for Structural Improvement
Weil, Joseph & Polhamus, Edward C.
May 28, 1951
Primary view of Aerodynamic characteristics with fixed and free transition of a modified delta wing in combination with fuselage at high subsonic speeds
Polhamus, Edward C. & King, Thomas J., Jr.
May 2, 1950
Primary view of Aerodynamic Damping at Mach Numbers of 1.3 and 1.6 of a Control Surface on a Two-Dimensional Wing by a Free-Oscillation Method
Tuovila, W. J. & Hess, Robert W.
May 1, 1956
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 Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effectiveness of an elevon as a longitudinal control and the effects of camber and twist on the maximum lift-drag ratio at supersonic speeds
Olson, Robert N. & Mead, Merrill H.
May 8, 1950
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Effects of split flaps, elevons, and leading-edge devices at low speed
Hopkins, Edward J.
May 19, 1949
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Investigation at a Mach number of 1.53 to determine the effects of cambering and twisting the wing for uniform load at a lift coefficient of 0.25
Madden, Robert T.
May 6, 1949
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
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