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Primary view of Tests of a triangular wing of aspect ratio 2 in the Ames 12-foot pressure wind tunnel. 1: the effect of Reynolds number and Mach number on the aerodynamic characteristics of the wing with flap undeflected
Edwards, George G. & Stephenson, Jack D.
January 22, 1948
Primary view of Dynamic Longitudinal Stability and Control of Tandem Coupled Bomber-Fighter Airplane Models With Rigid and Pitch-Free Couplings
Grana, David C. & Hewes, Donald E.
January 22, 1951
Primary view of An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degree Sweepback: Force Characteristics of the Complete Configuration and Its Various Components at Mach Numbers of 1.40 and 1.59
Smith, Norman F. & Marte, Jack E.
January 22, 1951
Primary view of Investigation of two-stage air-cooled turbine suitable for flight at Mach number of 2.5 2: blade design
Miser, James W. & Stewart, Warner L.
January 22, 1957
Primary view of Drag Measurements at Transonic Speeds of NACA 65-009 Airfoils Mounted on a Freely Falling Body to Determine the Effects of Sweepback and Aspect Ratio
Mathews, Charles W. & Thompson, Jim Rogers
January 22, 1947
Primary view of Performance of Compressor of XJ-41-V Turbojet Engine, 4, Performance Analysis Over Range of Compressor Speeds from 5000 to 10,000 RPM
Creagh, John W. R. & Ginsburg, Ambrose
January 22, 1948
Primary view of Effect of Exhaust Pressure on the Cooling Characteristics of a Liquid-Cooled Engine
Doyle, Ronald B. & Desmon, Leland G.
January 22, 1947
Primary view of Effect of Various Blade Modifications on Performance of a 16-Stage High-Pressure-Ratio Axial-Flow Compressor 1 - Effect on Over-All Performance Characteristics of Decreasing Twelfth Through Fifteenth State Stator-Blade Angles 3 Degrees
Medeiros, Arthur A.; Hatch, James E. & Dugan, James F., Jr.
January 22, 1952
Primary view of Performance of the 19XB 10-Stage Axial-Flow Compressor with Altered Blade Angles
Downing, Richard M.; Finger, Harold B. & Roepcke, Fay A.
January 22, 1947
Primary view of Investigation of Drag and Static Longitudinal and Lateral Stability and Control Characteristics of 1/20-Scale Model of McDonnell F4H-1 Airplane at Mach Numbers of 1.57, 1.87, 2.16, and 2.53: Phase II Model
Carmel, Melvin M. & Turner, Kenneth L.
January 22, 1957
Primary view of Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds
Gillis, Clarence L. & Chapman, Rowe, Jr.
January 22, 1953
Primary view of Method of Estimating the Stick-Fixed Longitudinal Stability of Wing-Fuselage Configurations Having Unswept or Swept Wings
McLaughlin, Milton D.
January 22, 1952
Primary view of Hinge-moment characteristics for several tip controls on a 60 degree sweptback delta wing at Mach number 1.61
Czarnecki, K. R. & Lord, Douglas R.
January 22, 1953
Primary view of Wind-Tunnel Investigation of a Shielded Total-Pressure Tube at Transonic Speeds
Gracey, William; Pearson, Albin O. & Russell, Walter R.
January 22, 1952
Primary view of Summary of some effective aerodynamic twisting-moment coefficients of various wing-control configurations at Mach numbers from 0.6 to 1.7 as determined from rocket-powered models
Strass, H. Kurt
January 22, 1952
Primary view of Effects of Auxiliary and Ejector Pumping on the Mach Number Attainable in a 4 1/2- by 4 1/2-Inch Slotted Tunnel at Low Pressure Ratios
Dennard, John S. & Little, Barney H., Jr.
January 22, 1954
Primary view of Calculated Effect of Uranium Distribution on Reflector Control Effectiveness for a Water-Moderated Power Reactor
Fox, Thomas A. & Valerino, Michael F.
January 22, 1954
Primary view of Flight and Preflight Evaluation of an Automatic Thrust-Coefficient Control System in a Twin-Engine Ram-Jet Missile
Dettwyler, H. Rudolph & Trout, Otto F., Jr.
January 22, 1954
Primary view of Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22 : longitudinal characteristics of a triangular wing and canard
Boyd, John W. & Peterson, Victor L.
January 22, 1958
Primary view of Drag of Conical and Circular-Arc Boattail Afterbodies at Mach Numbers From 0.6 to 1.3
Silhan, Frank V. & Cubbage, James M., Jr.
January 22, 1957
Primary view of Pressure Distribution Over a Series of Related Afterbody Shapes as Affected by a Propulsive Jet at Transonic Speeds
Henry, Beverly Z., Jr. & Cahn, Maurice S.
January 22, 1957
Primary view of Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone-Cylinder-Flare Configuration in Free Flight at Mach Numbers Up to 4.7
Rumsey, Charles B. & Lee, Dorothy B.
January 22, 1958
Primary view of A Simulator Investigation of Factors Affecting the Design and Utilization of a Stick Pusher for the Prevention of Airplane Pitch-Up
Holleman, Euclid C. & Boslaugh, David L.
January 22, 1958
Primary view of Investigation of Vortex Movements About a Wing in Steady Subsonic Flow Undergoing a Large Angle-of-Attack Change in a Blast-Induced Gust
McFarland, Donald R. & Huber, Paul W.
January 22, 1958
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