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Primary view of Progress Report on AEC Contract on Research and Development Program on Scintillation Crystals: Period 1 January 1956 to 1 April 1956
Beadle, Robert
April 25, 1956
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 Rocket-Model Investigation of the Rolling Effectiveness of a Fighter-Type Wing-Control Configuration at Mach Numbers From
Strass, H. Kurt & Marley, Edward T.
February 25, 1952
Primary view of A Summary of Results Obtained During Flight Simulation of Several Aircraft Prototypes With Variable-Stability Airplanes
McNeill, Walter E. & Creer, Brent Y.
May 25, 1956
Primary view of Wind-Tunnel Investigation at Low Speed of the Yawing Stability Derivatives of a 1/10-Scale Model of the Douglas A4D-1 Airplane
Wolhart, Walter D. & Fletcher, H. S.
August 25, 1954
Primary view of A Preliminary Study of the Effect of Boric Oxide Deposits on the Performance of Two Selected Turbine Stator-Blade Shapes
Setze, Paul C. & Nusbaum, William J.
February 25, 1958
Primary view of De-Icing and Runback Characteristics of Three Cyclic Electric, External De-Icing Boots Employing Chordwise Shedding
Ruggeri, Robert S.
May 25, 1953
Primary view of Preliminary Data on Rain Deflection from Aircraft Windshields by Means of High-Velocity Jet-Air Blast
Ruggeri, Robert S.
July 25, 1955
Primary view of A Photographic Study of Freezing of Water Droplets Falling Freely in Air
Dorsch, Robert G. & Levine, Joseph
February 25, 1952
Primary view of Effects of Free-Flight Rocket-Model Booster-Adapter Configurations on the Aerodynamic Characteristics in Pitch and Sideslip of a Swept-Wing Fighter Airplane Model at a Mach Number of 2.01
Robinson, Ross B.
March 25, 1955
Primary view of The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin
Buell, Donald A. & Tinling, Bruce E.
October 25, 1956
Primary view of Wind-Tunnel Measurements at Subsonic Speeds of the Static and Dynamic-Rotary Stability Derivatives of a Triangular-Wing Airplane Model Having a Triangular Vertical Tail
Beam, Benjamin H.; Reed, Verlin D. & Lopez, Armando E.
April 25, 1955
Primary view of Wind-Tunnel Tests of a Series of Practice Bombs
Ward, Donald H.
October 25, 1957
Primary view of Model Ditching Investigations of Three Airplanes Equipped With Hydro-Skis
Fisher, Lloyd J.
April 25, 1950
Primary view of Flight Characteristics of a Wingless Rocket- Powered Model With Four Externally Mounted Air-to-Air Missiles at Mach Numbers 0.7 to 1.6
Henning, Allen B. & Brown, Clarence A., Jr.
January 25, 1955
Primary view of Flight Test of an End-Burning Solid-Fuel Ramjet
Bartlett, Walter A., Jr.
March 25, 1954
Primary view of Exploratory Investigation of Performance of Experimental Fuel-Rich Hydrogen Combustion System
Smith, Arthur L. & Grobman, Jack S.
June 25, 1958
Primary view of The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings With 0 Degree and 45 Degree Sweep at Subsonic, Transonic, and Supersonic Speeds
Strass, H. Kurt
April 25, 1950
Primary view of Effect of combustion-chamber pressure and nozzle expansion ratio on theoretical performance of several rocket propellant systems
Morrell, Virginia E.
May 25, 1956
Primary view of Determination by the Free-Fall Method of the Drag and Longitudinal Stability and Control Characteristics of a Canard Model at Transonic Speeds
Kraft, Christopher C., Jr. & Mathews, Charles W.
August 25, 1950
Primary view of Effects of inlet icing on performance of axial-flow turbojet engine in natural icing conditions
Acker, Loren W. & Kleinknecht, Kenneth S.
May 25, 1950
Primary view of Investigation at Mach Number 1.62 of the Pressure Distribution Over a Rectangular Wing With Symmetrical Circular-Arc Section and 30-Percent-Chord Trailing-Edge Flap
Czarnecki, K. R. & Mueller, James N.
January 25, 1950
Primary view of Wing-flow measurements of longitudinal stability and control characteristics of a canard airplane configuration with a 45 degree sweptback wing and a triangular all-movable control surface
Crane, Harold L. & Adams, James J.
August 25, 1950
Primary view of Lift and drag coefficients for the Bell X-1 airplane (8-percent-thick wing) in power-off transonic flight
Carman, L. Robert & Carden, John R.
June 25, 1951
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