Technical Report Archive & Image Library (TRAIL) - 27 Matching Results

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Primary view of Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees: effect of Reynolds number at supersonic Mach numbers on the longitudinal characteristics of a wing twisted and cambered for uniform load
Heitmeyer, John C.
October 9, 1950
Primary view of An Air-Borne Densitometer for Smoke Concentration Measurements
Dvorak, R. V. & Chase, R. L.
October 9, 1951
Primary view of Altitude cooling investigation of the R-2800-21 engine in the P-47G airplane 2: investigation of the engine & airplane variables affecting the cylinder temperature distribution
Pesman, Gerard J. & Kaufman, Samuel J.
October 9, 1946
Primary view of Altitude cooling investigation of the R-2800-21 engine in the P-47g airplane 3: individual-cylinder temperature reduction by means of intake-pipe throttle and by coolant injection
Bell, E. Barton; Valerino, Michael F. & Manganiello, Eugene J.
October 9, 1946
Primary view of Analysis of longitudinal stability and trim of the Bell X-1 airplane at a lift coefficient of 0.3 to Mach numbers near 1.05
Drake, Hubert M.; Carden, John R. & Clagett, Harry P.
October 9, 1951
Primary view of Analysis of Turbine Stator Adjustment Required for Compressor Design-Point Operation in High Mach Number Supersonic Turbojet Engines
English, Robert E. & Cavicchi, Richard H.
October 9, 1953
Primary view of An analytical study of the comparative performance of six air-induction systems for turbojet-powered airplanes designed to operate at Mach numbers up to 2.0
Watson, Earl C.
October 9, 1953
Primary view of Comparison of several methods of predicting the pressure loss at altitude across a baffled aircraft-engine cylinder
Neustein, Joseph & Schafer, Louis J., Jr.
October 9, 1945
Primary view of Component Tests to Determine the Aerodynamic Characteristics of an All-Moveable 70 Degree Delta Canard-Type Control in the Presence of a Body at a Mach Number of 1.61
Spearman, M. Leroy
October 9, 1953
Primary view of Contaminant Effects Study : Phase Report, January 5 to September 15, 1962
Lieberman, A.
October 9, 1962
Primary view of Dynamic Stability and Control Characteristics of a Delta-Wing Vertically Rising Airplane Model in Take-Offs, Landings, and Hovering Flight
Lovell, Powell M., Jr.; Bates, William R. & Smith, Charles C., Jr.
October 9, 1951
Primary view of Effect of flame-holder design on altitude performance of louvered-liner afterburner
Renas, Paul E. & Jansen, Emmert T.
October 9, 1953
Primary view of A flight study of the effects on tracking performance of changes in the lateral-oscillatory characteristics of a fighter airplane
McNeill, Walter E.; Drinkwater, Fred J., III & Van Dyke, Rudolph D., Jr.
October 9, 1953
Primary view of Free Spinning and Recovery Characteristics of 1/36-Scale Model of the Republic F-105B Airplane
Bowman, James S., Jr.
October 9, 1957
Primary view of Geophysical Field Measurements for the U12e.10 Tunnel, Nevada Test Site, with a Discussion on the Generation of Shear Waves
Carroll, Roger D.; Muller, D. C. & Cunningham, M. J.
October 9, 1967
Primary view of Hazards Report for SM-1 Core II With the SM-1 Core II High Burnup Elements Replaced with SM-1 Core I Spare Elements
Coombe, J. R.; Lee, D. H. & Matthews, F. T.
October 9, 1961
Primary view of Model flight investigation of a nonlifting winged tow target
Shanks, Robert E.
October 9, 1950
Primary view of Performance of 4600-Pound-Thrust Centrifugal-Flow-Type Turbojet Engine With Water-Alcohol Injection at Inlet
Glasser, Philip W.
October 9, 1950
Primary view of Positioning Investigation of Single Slotted Flaps on a 47.7 Degrees Sweptback Wing at Reynolds Numbers of 4.0 X 10(Exp 6) and 6.0 X 10(Exp 6)
Spooner, Stanley H. & Mollenberg, Ernst F.
October 9, 1950
Primary view of Present Status of Aircraft Instruments
Subcommittee on Instruments
October 9, 1930
Primary view of A Reconnaissance For Oil Near Quanah, Hardeman County Texas
Wegemann, Carroll H.
October 9, 1915
Primary view of Rolling Effectiveness of All-Movable Wings at Small Angles of Incidence at Mach Numbers From 0.6 to 1.6
Strass, H. Kurt & Marley, Edward T.
October 9, 1951
Primary view of Sodium Reactor Experiment Power Expansion Program: Heat Transfer Systems Modifications
Freede, W. J. & Roberts, J. K.
October 9, 1964
Primary view of A theoretical investigation of the influence of autopilot natural frequency upon the dynamic performance characteristics of a supersonic canard missile configuration with a pitch-attitude control system
Passera, Anthony L.
October 9, 1951
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