National Advisory Committee for Aeronautics (NACA) - 509 Matching Results

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Primary view of Aerodynamic characteristics at subsonic and transonic speeds of a 42.7 degree sweptback wing model having an aileron with finite trailing-edge thickness
Turner, Thomas R.; Lockwood, Vernard E. & Vogler, Raymond D.
January 12, 1949
Primary view of Aerodynamic characteristics of 15 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. & Smith, Hamilton A.
October 1949
Primary view of Aerodynamic Characteristics of a 0.5-Scale Model of the Fairchild XSAM-N-2 Lark Missile at High Subsonic Speeds
Martin, Andrew & Hunter, Harlo A.
September 28, 1949
Primary view of Aerodynamic characteristics of a 6-percent-thick symmetrical double-wedge airfoil at transonic speeds from tests by the NACA wing-flow method
Lina, Lindsay J.
March 4, 1949
Primary view of Aerodynamic characteristics of a flying-boat hull having a length-beam ratio of 15 and a warped forebody
MacLeod, Richard G.
February 11, 1949
Primary view of Aerodynamic characteristics of a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: Transonic-bump method
Sleeman, William C., Jr. & Becht, Robert E.
April 21, 1949
Primary view of Aerodynamic Characteristics of a Wing With Quarter-Chord Line Swept Back 45 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section: Transonic-Bump Method
Weil, Joseph & Goodson, Kenneth W.
February 24, 1949
Primary view of Aerodynamic Characteristics of a Wing With Quarter-Chord Line Swept Back 45 Degrees, Aspect Ratio 6, Taper Ratio 0.6, and NACA 65A006 Airfoil Section
Goodson, Kenneth W. & Few, Albert G., Jr.
November 1, 1949
Primary view of Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 6, taper ratio 0.6, and NACA 65A009 airfoil section
Spreemann, Kenneth P.; Morrison, William D., Jr. & Pasteur, Thomas B., Jr.
July 20, 1949
Primary view of Aerodynamic characteristics of a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: transonic-bump method
King, Thomas J., Jr. & Myers, Boyd C., II
September 6, 1949
Primary view of Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section
Goodson, Kenneth W. & Morrison, William D., Jr.
October 21, 1949
Primary view of Aerodynamic Characteristics of an 0.08-Scale Model of the Martin XB-51 Airplane at High Subsonic Speeds
Barnes, Robert H.
October 7, 1949
Primary view of Aerodynamic Characteristics of an Airfoil-Forebody Swept Flying-Boat Hull With a Wing and Tail Swept Back 51.3 Degrees at the Leading Edge
Naeseth, Rodger L. & MacLeod, Richard G.
September 9, 1949
Primary view of Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)
Schaefer, Raymond F. & Smith, Hamilton A.
December 1949
Primary view of The aerodynamic characteristics throughout the subsonic speed range of a thin, sharp-edged horizontal tail of aspect ratio 4 equipped with a constant-chord elevator
Bandettini, Angelo & Reed, Verlin D.
June 30, 1949
Primary view of Aerodynamic Properties of Cruciform-Wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds
Spreiter, John R.
June 1949
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Aerodynamic characteristics in sideslip of a large-scale model having a 63 degree swept-back vertical tail
McCormack, Gerald M.
October 7, 1949
Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Characteristics at a Mach number of 1.53 including effect of small variations of sweep
Madden, Robert T.
January 26, 1949
Primary view of Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept Back 63 Degrees: Characteristics for Symmetrical Wing Sections at High Subsonic and Moderate Supersonic Mach Numbers
Mas, Newton A.
July 7, 1949
Primary view of Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept Back 63 Degrees: Characteristics Throughout the Subsonic Speed Range With the Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25
Jones, J. Lloyd & Demele, Fred A.
August 15, 1949
Primary view of Aerodynamic Study of a Wing-Fuselage Combination Employing a Wing Swept Back 63 Degrees: Effects at Subsonic Speeds of a Constant-Chord Elevon on a Wing Cambered and Twisted for a Uniform Load at a Lift Coefficient of 0.25
Jones, J. Lloyd & Demele, Fred A.
December 5, 1949
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 Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: Investigation of a large-scale model at low speed
McCormack, Gerald M. & Walling, Walter C.
January 21, 1949
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