National Advisory Committee for Aeronautics (NACA) - 5,157 Matching Results

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Primary view of Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01
Spearman, M. Leroy
October 30, 1953
Primary view of Aerodynamic characteristics including effects of wing fixes of a 1/20-scale model of the Convair F-102 airplane at transonic speeds
Osborne, Robert S. & Wornom, Dewey E.
March 18, 1954
Primary view of Aerodynamic characteristics including pressure distribution of a fuselage and three combinations of the fuselage with swept-back wings at high subsonic speeds
Sutton, Fred B. & Martin, Andrew
February 6, 1951
Primary view of Aerodynamic Characteristics Including Scale Effect of Several Wings and Bodies Alone and in Combination at a Mach Number of 1.53
Van Dyke, Milton D.
December 20, 1946
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 0.04956-Scale Model of the Convair F-102A Airplane at Mach Numbers of 1.41, 1.61, and 2.01
Spearman, M. Leroy & Driver, Cornelius
September 30, 1955
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Transonic Speeds
Tempelmeyer, Kenneth E. & Osborne, Robert S.
April 11, 1955
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102B Airplane at Mach Numbers of 1.41, 1.61, and 2.01: Coord No. AF-231
Driver, Cornelius & Robinson, Ross B.
February 7, 1956
Primary view of Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair TF-102A Airplane at Transonic Speeds, Coord. No. AF-120
Osborne, Robert S.
1957~
Primary view of Aerodynamic Characteristics of a 1/4-Scale Model of the Duct System for the General Electric P-1 Nuclear Powerplant for Aircraft
Wood, Charles C. & Henry, John R.
July 29, 1955
Primary view of Aerodynamic Characteristics of a 6-Percent-Thick Symmetrical Circular-Arc Airfoil Having a 30-Percent-Chord Trailing-Edge Flap at a Mach Number of 6.9
Ridyard, Herbert W. & Fetterman, David E., Jr.
June 5, 1956
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 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 45 Degree Swept-Back Wing With Aspect Ratio of 3.5 and NACA 2S-50(05)-50(05) Airfoil Sections
Proterra, Anthony J.
August 4, 1947
Primary view of Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept-Wing Fighter-Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic characteristics of a 60 degree delta wing having a half-delta tip control at a Mach number of 4.04
Ulmann, Edward F. & Smith, Fred M.
April 25, 1955
Primary view of Aerodynamic characteristics of a 68.4 degree delta wing at Mach numbers of 1.6 and 1.9 over a wide Reynolds number range
Hatch, John E., Jr. & Gallagher, James J.
November 2, 1953
Primary view of The aerodynamic characteristics of a body in the two-dimensional flow field of a circular-arc wing at a Mach number of 2.01
Gapcynski, John P. & Carlson, Harry W.
July 2, 1957
Primary view of Aerodynamic characteristics of a canard and an outboard-tail airplane model at a Mach number of 2.01
Spearman, M. Leroy & Robinson, Ross B.
March 24, 1958
Primary view of Aerodynamic Characteristics of a Circular Cylinder at Mach Number 6.86 and Angles of Attack Up to 90 Degrees
Penland, Jim A.
March 11, 1954
Primary view of Aerodynamic characteristics of a cruciform-wing missile with canard control surfaces and of some very small span wing-body missiles at a Mach number of 1.41
Spearman, M. Leroy & Robinson, Ross B.
April 12, 1954
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 Flying-Boat Hull Having a Length-Beam Ratio of 15, TED No. NACA 2206
Riebe, John M. & Naeseth, Rodger L.
January 23, 1951
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