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Primary view of Preliminary performance data for the J57-P-1 turbojet engine at altitudes up to 65,000 feet
Miller, Robert R. & Bloomer, Harry E.
June 15, 1954
Primary view of Characteristics of a Hydraulic Control Determined from Transient Data Obtained with a Turbojet Engine at Altitude
Vasu, George; Hinde, William L. & Craig, R. T.
June 16, 1954
Primary view of Effect of Mechanically Induced Sinusoidal Air-Foil Oscillations on Operation of a Ram-Jet Engine
Dangle, E. E.; Cervenka, A. J. & Perchonok, Eugene
June 16, 1954
Primary view of Performance of mixed-flow impeller, model MFI-1B, with diffuser vanes at equivalent impeller speeds from 1100 to 1700 feet per second
Osborn, Walter M.
June 16, 1954
Primary view of Results of an Airborne Radiometric Survey in the Canon City Embayment Area, Colorado
Nash, A. L. & Brown, L. J.
June 16, 1954
Primary view of Table Top Ion Source
Ford, Franklin O. & Zizzo, Samuel G.
June 16, 1954
Primary view of Drag and Heat Transfer on a Parabolic Body of Revolution (NACA RM-10) in Free Flight to Mach Number 2 With Both Constant and Varying Reynolds Number and Heating Effects on Turbulent Skin Friction
Maloney, Joseph P.
June 17, 1954
Primary view of Dual Channel Pulse Analyser and Count-Rate Meter for Gamma Spectrometer Monitor
Paul, R. S. & Wood, M. R.
June 17, 1954
Primary view of Flight Investigation of the Aerodynamic Derivatives and Performance of Control Systems of Two Full-Scale Guided Bombs
Seaberg, Ernest C. & Geller, Edward S.
June 17, 1954
Primary view of Flight Investigation to Determine Lift and Drag Characteristics of a Canard Ram-Jet Missile Configuration in the Mach Number Range of 0.8 to 2.0
Gammal, Abraham A. & Kennedy, Thomas L.
June 17, 1954
Primary view of An Investigation of the Effects of Jet Exhaust and Reynolds Number Upon the Flow Over the Vertical Stabilizer and Rudder of the Douglas D-558-II Research Airplane at Mach Numbers of 1.62, 1.93, and 2.41
Grigsby, Carl E.
June 17, 1954
Primary view of Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data
Burrows, Dale L.
June 17, 1954
Primary view of Summary of Turbulence Data Obtained During United Air Lines Flight Evaluation of an Experimental C Band (5.5 cm) Airborne Weather Radar
Coe, E. C. & Fetner, M. W.
June 17, 1954
Primary view of Effect of wing flexibility on the damping roll of a notched delta-wing body combination between Mach numbers 0.6 and approximately 2.2 as determined with rocket-propelled models
Bland, William M., Jr.
June 18, 1954
Primary view of Transonic Flight Test of a Rocket-Powered Model to Determine Propulsive Jet Influence on the Configuration Drag
deMoraes, Carlos A.
June 18, 1954
Primary view of Analysis of Factors Affecting Selection and Design of Air-Cooled Single-Stage Turbines for Turbojet Engines 2: Analytical Techniques
Rossbach, Richard J.
June 21, 1954
Primary view of Effect of immersed surfaces in combustion zone on efficiency and stability of 5-inch diameter ram-jet combustor
Reynolds, Thaine W. & Male, Donald W.
June 21, 1954
Primary view of Effect of Nozzle Contour on Drag of Parabolic Afterbodies
Vargo, Donald J. & Englert, Gerald W.
June 21, 1954
Primary view of A Wind-Tunnel Investigation of the Use of Spoilers for Obtaining Static Longitudinal Stability of a Canard-Missile Model in Reverse Flight
Fletcher, Herman S.
June 21, 1954
Primary view of A study of the use of controls and the resulting airplane response during service training operations of four jet fighter airplanes
Mayer, John P.; Hamer, Harold A. & Huss, Carl R.
June 22, 1954
Primary view of Take-Off and Landing Characteristics of a 0.13-Scale Model of the Convair XFY-1 Vertically Rising Airplane in Steady Winds, TED No. NACA DE 368
Schade, Robert O.; Smith, Charles C., Jr. & Lovell, P. M., Jr.
June 22, 1954
Primary view of Investigation of the Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 2.02
Bressette, Walter E.
June 23, 1954
Primary view of Investigation of the Normal Force Accompanying Thrust-Axis Inclination of the NACA 1.167-(0)(03)-058 and the NACA 1.167-(0)(05)-058 Three-Blade Propellers at Forward Mach Numbers to 0.90
Demele, Fred A. & Otey, William R.
June 23, 1954
Primary view of A Preliminary Investigation of the Pressure Recovery of Several Two-Dimensional Supersonic Inlets at Mach Number of 2.01
Comenzo, Raymond J.
June 23, 1954
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