National Advisory Committee for Aeronautics (NACA) - 13,786 Matching Results

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Primary view of Some Effects of Flow Spoilers and of Aerodynamic Balance on the Oscillating Hinge Moments for a Swept Fin-Rudder Combination in a Transonic Wind Tunnel
Herr, Robert W.; Gibson, Frederick W. & Osborne, Robert S.
May 28, 1958
Primary view of Analyses for Turbojet Thrust Augmentation With Fuel-Rich Afterburning of Hydrogen, Diborane, and Hydrazine
Morris, James F.
June 18, 1957
Primary view of Wing Pressure Distributions Over the Lift Range of the Convair XF-92A Delta-Wing Airplane at Subsonic and Transonic Speeds
Keener, Earl R. & Jordan, Gareth H.
November 30, 1955
Primary view of Evolution of the Helicopter
Balaban, Karl
March 1923
Primary view of Determination of Rate, Area, and Distribution of Impingement of Waterdrops on Various Airfoils From Trajectories Obtained on the Differential Analyzer
Guibert, A. G.; Janssen, E. & Robbins, W. M.
February 16, 1949
Primary view of Experimental Investigation of a New Type of Low-Drag Wing-Nacelle Combination
Allen, H. Julian & Frick, Charles W., Jr.
July 1942
Primary view of Wind-Tunnel Investigation of Mutual Interference Loads on a Supersonic Bomber Configuration and Store During Separation at Mach Numbers of 1.57, 1.77, and 2.01
Morris, Owen G. & Turner, Kenneth L.
October 25, 1957
Primary view of Stability and Control Characteristics at Low Speed of a 1/10-Scale Model of MX-1554A Design
Lockwood, Vernard E. & Solomon, Martin
1953
Primary view of Static Lateral and Directional Stability and Control Characteristics of a Revised 1/22-Scale Model of the Republic F-105 Airplane at Mach Numbers of 1.41 and 2.01
Robinson, Ross B. & Foster, Gerald V.
October 16, 1956
Primary view of Some Effects of Aeroelasticity on the Rolling Effectiveness of a 10-Percent-Scale Model of the Mcdonnell F-101A Airplane Wing at Mach Numbers From 0.5 to 1.2
English, Roland D.
September 2, 1955
Primary view of Stability and Control Characteristics at Low Speed of a Modified 1/10-Scale Model of the MX-1554A Design
Lockwood, Vernard E. & Solomon, Martin
November 9, 1953
Primary view of Stability and Control Characteristics at High Subsonic Speeds of a 1/30-Scale Model of the MX-1554A Design
Lockwood, Vernard E.; Luoma, Arvo A. & Solomon, Martin
October 29, 1953
Primary view of Speed-Brake Investigation at Low Speed of a 1/10-Scale Model of the MX-1554A Airplane With a Circular Jet Nozzle
Solomon, Martin
January 7, 1954
Primary view of Investigation of Drag and Static Longitudinal and Lateral Stability Characteristics of a 1/15-Scale Model of the Grumman F11F-1F Airplane at Mach Numbers of 1.56, 1.76, 2.06, and 2.53
Turner, Kenneth L. & Fournier, Roger H.
November 30, 1956
Primary view of Investigation of the Low-Speed Flight Characteristics of a 1/15-Scale Model of the Convair XB-58 Airplane
Paulson, John W.
November 14, 1957
Primary view of Free-Spinning-Tunnel Investigation of a 1/28-Scale Model of the North American FJ-4 Airplane
Healy, Frederick M.
January 13, 1958
Primary view of Preliminary Wind-Tunnel Investigation of the Performance of Republic F-105 Wing-Root Inlet Configurations at Various Angles of Attack and a Mach Number of 2.01
Kouyoumjian, Walter L.
January 15, 1957
Primary view of Summary and Analysis of Horizontal-Tail Contribution to Longitudinal Stability of Swept-Wing Airplanes at Low Speeds
Neely, Robert H. & Griner, Roland F.
August 23, 1955
Primary view of Transonic Aerodynamic and Trim Characteristics of 1/15-Scale Models of the Convair MX-1964 Airplane With Indented Fuselage
Allis, Arthur E.; Swihart, John M. & Foss, Willard E., Jr.
1953
Primary view of Low-Speed Wind-Tunnel Tests of a 1/8-Scale Model of the Bell D-188A VTOL Airplane
McKinney, Marion O. & Smith, Charles C., Jr.
August 1, 1958
Primary view of A Wind-Tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds
Heath, Atwood R., Jr. & Igoe, Ann W.
July 21, 1958
Primary view of Wind-Tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-Wing Airplane With Blowing Flaps and Leading-Edge Slats
James, Harry A. & Maki, Ralph L.
July 5, 1957
Primary view of Aerodynamic Characteristics of Two Rectangular-plan-form, Allmovable Controls in Combination With a Slender Body of Revolution at Mach Numbers From 3.00 to 6.25
Wong, Thomas J. & Gloria, Hermilo R.
December 28, 1955
Primary view of An Analysis of a Nuclear Powered Supercritical-Water Cycle for Aircraft Propulsion
Karp, Irving M.
January 19, 1953
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