National Advisory Committee for Aeronautics (NACA) - 185 Matching Results

Search Results

Results: 1 - 24 next
Primary view of Experimental Flutter Results for Cantilever-Wing Models at Mach Numbers Up to 3.0
Tuovila, W. J. & McCarty, John Locke
June 14, 1955
Primary view of A preliminary investigation of the use of circulation control to increase the lift of a 45 degree sweptback wing by suction through trailing-edge slots
Cook, Woodrow L.; Griffin, Roy N., Jr. & Hickey, David H.
December 14, 1954
Primary view of Some effects of aileron span, aileron chord, and wing twist on rolling effectiveness as determined by rocket-powered model tests and theoretical estimates
Strass, H. Kurt & Tucker, Warren A.
September 14, 1954
Primary view of Aspects of internal-flow-system design for helicopter propulsive units
Henry, John R.
September 14, 1954
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 Investigation of Control Effectiveness and Stability Characteristics of a Model of a Low-Wing Missile With Interdigitated Tail Surfaces at Mach Numbers of 2.29, 2.97, and 3.51
Presnell, John G., Jr.
July 14, 1958
Primary view of Effects of Boattail Area Contouring and Simulated Turbojet Exhaust on the Loading and Fuselage-Tail Component Drag of a Twin-Engine Fighter-Type Airplane Model
Foss, Willard E., Jr.; Runckel, Jack F. & Lee, Edwin E., Jr.
July 14, 1958
Primary view of Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at Mach numbers from 0 to 1.9
Lazzeroni, Frank A. & Pfyl, Frank A.
February 14, 1956
Primary view of Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections
Berggren, Robert E. & Graham, Donald J.
April 14, 1954
Primary view of Investigation of a 1/4 Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control and Horizontal-Tail Hinge-Moment and Normal-Force Characteristics of the Model Equipped With a Drooped Supersonic-Type Elliptical Wing-Root Inlet
Cancro, Patrick A. & Kelly, H. Neale
November 14, 1955
Primary view of Power-Off Tests of the Northrop N9M-2 Tailless Airplane in the 40- by 80-Foot Wind Tunnel
Stevens, Victor I., Jr. & McCormack, Gerald M.
December 14, 1944
Primary view of Experimental Static Aerodynamic Forces and Moments at High Subsonic Speeds on a Canard Missile During Simulated Launching From the Midsemispan Location of a 45 Degree Sweptback Wing-Fuselage-Pylon Combination at Zero Sideslip
Alford, William J., Jr. & King, Thomas J., Jr.
January 14, 1957
Primary view of Preliminary Analysis of Hydrogen-Rich Hypersonic Ramjet Operation
Breitwieser, Roland & Morris, James F.
January 14, 1958
Primary view of An Investigation of the Longitudinal Stability Characteristics of Three Specialized Store Configurations at Transonic Speeds
Braden, John A.
January 14, 1955
Primary view of Experimental and Analytical Study of Balanced-Diaphragm Fuel Distributors for Gas-Turbine Engines
Straight, David M. & Gold, Harold
August 14, 1950
Primary view of Aerodynamic Forces and Moments on a Large Ogive-Cylinder Store at Various Locations Below the Fuselage Center Line of a Swept-Wing Bomber Configuration at a Mach Number of 1.61
Morris, Odell A.
January 14, 1957
Primary view of Investigation of Afterburner Combustion Screech and Methods of Its Control at High Combustor Pressure Levels
Trout, Arthur M.; Koffel, William K. & Smolak, George R.
May 14, 1956
Primary view of Hydrodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane Designed for Supersonic Flight
Coffee, Claude W., Jr.
July 14, 1958
Primary view of Simulated Flight Investigation of Scaled-Speed Elastic Sweptwing Bomber and Fighter Models Coupled Wing Tip to Wing Tip
Thompson, Robert F.
February 14, 1956
Primary view of Transonic Flutter Investigation of an All-Movable Horizontal Tail for a Fighter Airplane
Land, Norman S. & Abbott, Frank T., Jr.
January 14, 1957
Primary view of Estimate of Hull-Weight Change with Varying Length-Beam Ratio for Flying Boats
Benscoter, Stanley U.
August 14, 1947
Primary view of Indirect Methods for Obtaining Ram-Jet Exhaust-Gas Temperature Applied to Fuel-Metering Control
Perchonok, Eugene; Sterbentz, William H. & Moore, Stanley H.
January 14, 1948
Primary view of A Low-Speed Investigation of an Annular Transonic Air Inlet
Nichols, Mark R. & Rinkoski, Donald W.
April 14, 1947
Primary view of Flight Investigation of a 20-Inch-Diameter Steady-Flow Ram Jet
Disher, John H.
January 14, 1948
Back to Top of Screen