Technical Report Archive & Image Library (TRAIL) - 920 Matching Results

Search Results

Results: 1 - 24 next
Primary view of 3 Plant Radiation Study Interim Report #5- Part II Data on Gamma Shielding of Special Plutonium Samples
Moulthrop, H. A.
October 22, 1959
Primary view of The Absorption Spectra of Complexes of Uranium (VI) with Some [beta]-Diketones
Feinstein, H. I.
October 1956
Primary view of Accelerator Development Department Internal Report
Blewett, J. P.
October 2, 1958
Primary view of Accuracy of Volume Measurements in a Large Process Vessel
Pleasance, C. L.
October 19, 1959
Primary view of The Activation of Low-Reactivity Uranium Dioxide Particles
Bard, R. J.; Bunker, D. L.; Greenough, R. C. & Kalmus, E. H.
October 1955
Primary view of Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hydro-ski aircraft with a variable-incidence wing
Petynia, William W.; Hasson, Dennis F. & Spooner, Stanley H.
October 23, 1957
Primary view of The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
Chang, Chieh-Chien
October 1951
Primary view of Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-Chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees
Kemp, William B., Jr.; Goodson, Kenneth W. & Booth, Robert A.
October 10, 1950
Primary view of Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01
Spearman, M. Leroy
October 30, 1953
Primary view of Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7
Turner, M. J. & Rabinowitz, S.
October 1950
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 Air Core Cryogenic Magnet Coils for Fusion Research and High Energy Nuclear Physics Applications
Post, Richard F. & Taylor, C. E.
October 30, 1959
Primary view of Air-flow characteristics of brazed and rolled wire filter cloth for transpiration-cooled afterburners
Koffel, William K.
October 26, 1953
Primary view of An air-flow-direction pickup suitable for telemetering use on pilotless aircraft
Ikard, Wallace L.
October 1956
Primary view of Airborne radiometric survey of upper Michigan and parts of Wisconsin
Smith, Burton C. & Fickel, Clarence W.
October 16, 1957
Primary view of Aircraft Nuclear Propulsion Project Quarterly Progress Report for Period Ending June 10, 1952
Briant, R. C.; Buck, J. H.; Miller, A. J. & Cottrell, William B.
October 23, 1952
Primary view of Altitude evaluation of several afterburner design variables on a J47-GE-17 turbojet engine
Braithwaite, Willis M.; Walker, Curtis L. & Sivo, Joseph N.
October 23, 1953
Primary view of Altitude-ignition limit of a turbojet engine using a condenser-discharge ignition system
Armstrong, John C.
October 23, 1951
Primary view of Altitude investigation of performance of turbine-propeller engine and its components
Wallner, Lewis E. & Saari, Martin J.
October 5, 1950
Primary view of Amendment No. 2 To License Application For Nuclear Test Reactor
General Electric Company
October 7, 1958
Primary view of Amplitude of Supersonic Diffuser Flow Pulsations
Sterbentz, William H. & Davids, Joseph
October 1955
Primary view of Analog computer study of some filtering, command-computer, and automatic-pilot problems connected with the attack phase of the automatically controlled supersonic interceptor
Sherman, Windsor L.
October 3, 1957
Primary view of Analogy Between Mass and Heat Transfer with Turbulent Flow
Callaghan, Edmund E.
October 1953
Back to Top of Screen