Technical Report Archive & Image Library (TRAIL) - 26 Matching Results

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Primary view of Analysis of Factors Affecting Selection and Design of Air-Cooled Single-Stage Turbine for Turbojet Engines 1: Turbine Performance and Engine Weight-Flow Capacity
Rossbach, Richard J.; Schramm, Wilson B. & Hubbartt, James E.
May 25, 1954
Primary view of Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 : Supplement I - Influence of new boric-oxide vapor-pressure data on calculated performanc
Tower, Leonard K.
May 25, 1956
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 Effect of rotor- and stator-blade modifications on surge performance of an 11-stage axial-flow compressor 2: redesigned compressor for XJ-40-WE-6 engine
Conrad, E. William; Finger, Harold B. & Essig, Robert H.
May 25, 1953
Primary view of The Effect of Wing Fences on the Longitudinal Characteristics at High Subsonic Speeds of a Wing-Fuselage-Tail Combination Having a Wing With 40 Degrees of Sweepback and NACA Four-Digit Thickness Distribution
Dickson, Jerald K. & Sutton, Fred B.
May 25, 1955
Primary view of The effect of wing height on the longitudinal characteristics at high subsonic speeds of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and NACA four digit thickness distribution
Dickson, Jerald K. & Sutton, Fred B.
May 25, 1955
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 Effects of spanwise location of sweep discontinuity on the low-speed static lateral stability characteristics of a complete model with wings of M and W plan form
Fournier, Paul G.
May 25, 1955
Primary view of Experimental investigation of the effect of a shrouded rotor on the performance of a conservatively designed turbine
Hauser, Cavour H. & Plohr, Henry W.
May 25, 1954
Primary view of Experimental Static Aerodynamic Forces and Moments at Low Speed on a Missile Model During Simulated Launching From the 25-Percent-Semispan and Wing-Tip Location of a 45 Degree Sweptback Wing-Fuselage Combination
Alford, William J., Jr.; Silvers, H. Norman & King, Thomas J., Jr.
May 25, 1955
Primary view of Flight measurements of wing loads on the Convair XF-92A delta-wing airplane
Kuhl, Albert E. & Johnson, Clinton T.
May 25, 1955
Primary view of Free-Jet Altitude Investigation of a 20-Inch Ram-Jet Combustor With a Rich Inner Zone of Combustion for Improved Low-Temperature-Ratio Operation
Trout, Arthur M. & Wentworth, Carl B.
May 25, 1953
Primary view of A horizontal-tail arrangement for counteracting static longitudinal instability of sweptback wings
Edwards, George G. & Savage, Howard F.
May 25, 1956
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 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 Investigation of a high-temperature single-stage turbine suitable for air cooling and turbine stator adjustment 1: design of vortex turbine and performance with stator at design setting
Heaton, Thomas R.; Forrette, Robert E. & Holeski, Donald E.
May 25, 1954
Primary view of Investigation of annular liquid flow with concurrent air flow in horizontal tubes
Kinney, George R. & Abramson, Andrew E.
May 25, 1951
Primary view of Limits of Flammability of Pure Hydrocarbon-Air Mixtures at Reduced Pressures and Room Temperature
DiPiazza, James T.
May 25, 1951
Primary view of Low-Speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing
Sleeman, William C., Jr. & Alford, William J., Jr.
May 25, 1955
Primary view of The N.A.C.A. photographic apparatus for studying fuel sprays from oil engine injection valves and test results from several researches
Beardsley, Edward G.
May 25, 1927
Primary view of Photographic Study of Rotary Screaming and Other Oscillations in a Rocket Engine
Male, Theodore; Kerslake, William R. & Tischler, Adelbert O.
May 25, 1954
Primary view of Preliminary Investigation at a Mach Number of 1.9 and a Reynolds Number of 2,200,000 of Three Ailerons Applicable to the Bell XS-2 Airplane Design
Sivells, James C. & Conner, D. William
May 25, 1948
Primary view of Preliminary investigation of short two-dimensional subsonic diffusers
Woollett, Richard R.
May 25, 1956
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
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