Technical Report Archive & Image Library (TRAIL) - 208 Matching Results

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Primary view of Acceleration Measurements During Landings of a 1/5.5-Size Dynamic Model of the Columbia XJL-1 Amphibian in Smooth Water and in Waves: Langley Tank Model 208M, TED No. NACA 2336
Clement, Eugene P. & Havens, Robert F.
September 25, 1947
Primary view of Additional measurements of the low-speed static stability of a configuration employing three triangular wing panels and a body of equal length
Delany, Noel K.
July 25, 1955
Primary view of Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-Body Combinations Having Cambered Wings With an Aspect Ratio of 3.5 and a Taper Ratio of 0.2: Effect at M = 2.01 of Nacelle Shape and Position on the Aerodynamic Characteristics in Pitch of Two Wing-Body Combinations with 47 Degree Sweptback Wings
Driver, Cornelius
July 25, 1952
Primary view of Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full-Span Flap Type of Control With Overhang Balance: Transonic-Bump Method
Lockwood, Vernard E. & Hagerman, John R.
January 25, 1952
Primary view of Aerodynamic characteristics of a 60 degree delta wing having a half-delta tip control at a Mach number of 4.04
Ulmann, Edward F. & Smith, Fred M.
April 25, 1955
Primary view of Aerodynamic Characteristics of Missile Configurations With Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01
Robinson, Ross B.
June 25, 1957
Primary view of Aerodynamics of slender bodies at Mach number of 3.12 and Reynolds numbers from 2 x 10(exp 6) to 15 x 10(exp 6) 4: aerodynamic characteristics of series of four bodies having near-parabolic noses and cylindrical afterbodies
Jack, John R. & Moskowitz, Barry
January 25, 1954
Primary view of Altitude-Wind-Tunnel Investigation of the 19B-2, 19B-8 and 19XB-1 Jet- Propulsion Engines: 4 - Analysis of Compressor Performance
Dietz, Robert O. & Kuenzig, John K.
April 25, 1947
Primary view of Altitude-wind-tunnel investigations of thrust augmentation of a turbojet engine 1: Performance with tail-pipe burning
Fleming, W. A. & Dietz, R. O.
September 25, 1946
Primary view of The Ames supersonic free-flight wind tunnel
Seiff, Alvin; James, Carlton S.; Canning, Thomas N. & Boissevain, Alfred G.
April 25, 1952
Primary view of The Ames Supersonic Free-Flight Wind Tunnel
Seiff, Alvin; James, Carlton S.; Canning, Thomas N. & Boissevain, Alfred G.
April 25, 1952
Primary view of Analysis of cooling-air requirements of corrugated-insert-type turbine blades suitable for a supersonic turbojet engine
Ziemer, Robert R. & Slone, Henry O.
April 25, 1956
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 An analysis of longitudinal-control problems encountered in flight at transonic speeds with a jet-propelled airplane
Brown, Harvey H.; Rolls, L. Stewart & Clousing, Lawrence A.
September 25, 1947
Primary view of Analysis of V-G records from ten types of Navy airplanes in squadron operations during the period 1949 to 1953
Mayer, John P. & Harris, Agnes E.
March 25, 1955
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 Analytical determination of effect of turbine cooling-air-impeller performance on engine performance and comparison of experimentally determined performance of impellers with and without inducer vanes
Schafer, Louis J., Jr. & Hickel, Robert O.
October 25, 1954
Primary view of Analytical investigation of factors affecting the performance of single-stage turbines having rotor-tip discharge of cooling air
Smith, Gordon T. & Hickel, Robert O.
April 25, 1956
Primary view of Applications of auxiliary air injectors to supersonic wind tunnels
Spiegel, Joseph M.; Hofstetter, Robert U. & Kuehn, Donald M.
November 25, 1953
Primary view of Bodies of Revolution for Minimum Drag at High Supersonic Airspeeds
Eggers, A. J., Jr.; Dennis, David H. & Resnikoff, Meyer M.
February 25, 1952
Primary view of Calculated and measured pressure distributions over the midspan section of the NACA 4412 airfoil
Pinkerton, Robert M.
March 25, 1936
Primary view of Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0
Brajnikoff, George B. & Rogers, Arthur W.
June 25, 1951
Primary view of Comparative flight performance with an NACA Roots supercharger and a turbocentrifugal supercharger
Schey, Oscar W. & Young, Alfred W.
February 25, 1930
Primary view of Comparison of Alcogas Aviation Fuel With Export Aviation Gasoline
Gage, V. R.; Sparrow, S. W. & Harper, D. R.
November 25, 1919
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