The Online Books Page

Books by Lewis Flight Propulsion Laboratory:

Books in the extended shelves:

• Lewis Flight Propulsion Laboratory: Altitude performance of an afterburner with pentaborane fuel (National Advisory Committee for Aeronautics, 1957), also by James W. Useller, David B. Fenn, J. Robert Branstetter, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: An analog study of a shock-position diffuser control on a supersonic turbojet engine (National Advisory Committee for Aeronautics, 1956), also by David Novik, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Analysis of compressor performance (National Advisory Committee for Aeronautics, 1948), also by Robert O. Dietz and John K. Kuenzig (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight Mach numbers of 0, 2.0, and 2.8 (National Advisory Committee for Aeronautics, 1954), also by Richard H. Cavicchi, Robert E. English, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: An analysis of ram-jet-engine time delay following a fuel-flow disturbance (National Advisory Committee for Aeronautics, 1955), also by Fred A. Wilcox, Arthur R. Anderson, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Analysis of turbine performance of 19B-8 engine (National Advisory Committee for Aeronautics, 1948), also by Richard P. Krebs and Frank L. Suozzi (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Analytical investigation of fuel temperatures and fuel-evaporation losses encountered in long-range high-altitude supersonic flight (National Advisory Committee for Aeronautics, 1953), also by Richard J. McCafferty (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Analytical investigation of two liquid cooling systems for turbine blades (National Advisory Committee for Aeronautics, 1951), also by Thomas W. Jackson and John N. B. Livingood (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: An analytical study of heat requirements for icing protection of radomes (National Advisory Committee for Aeronautics, 1953), also by James P. Lewis (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Analytical study of the equilibrium thickness of boric oxide deposits on jet-engine surfaces (National Advisory Committee for Aeronautics, 1957), also by Paul C. Setze, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Application of oblique-shock sensing system to ram-jet-engine flight Mach number control (National Aeronautics and Space Administration, 1955), also by Fred A. Wilcox, Donald P. Hearth, United States. National Adviosry Committee for Aeronautics, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Average bond energies between boron and elements of the fourth, fifth, sixth, and seventh groups of the periodic table (National Advisory Committee for Aeronautics, 1955), also by A. P. Altshuller, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Blade-to-coolant heat-transfer results and operating data from a natural-convection water-cooled single-stage turbine (National Advisory Committee for Aeronautics, 1951), also by Anthony J. Diaguila and John C. Freche (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Blow-out velocities of several slurry and liquid fuels in a 1 7/8-inch-diameter combustor (National Advisory Committee for Aeronautics, 1955), also by James F. Morris, Albert M. Lord, Robert M. Caves, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Carbon-deposition characteristics of MIL-F-5624A fuels containing high-boiling aromatic hydrocarbons (National Advisory Committee for Aeronautics, 1952), also by Edmund R. Jonash, William P. Cook, and Jerrold D. Wear (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Carbon deposition obtained with MIL-F-5624A fuels in a single combustor and in three full-scale engines (National Advisory Committee for Aeronautics, 1954), also by Jerrold D. Wear (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Carbon deposition of several special turbojet-engine fuels (National Advisory Committee for Aeronautics, 1951), also by Jerrold D. Wear and James W. Useller (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Chemical and physical factors affecting combustion in fuel : nitric acid systems (National Advisory Committee for Aeronautics, 1958), also by James Baker and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Combustion-chamber performance (National Advisory Committee for Aeronautics, 1948), also by Bemrose Boyd (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Combustion-chamber performance with four fuels in bumblebee 18-inch ram jet incorporating various rake- or gutter-type flame holders (National Advisory Committee for Aeronautics, 1948), also by Ephraim M. Howard, David T. Dupree, and Fred A. Wilcox (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Combustion of aluminum borohydride in a supersonic wind tunnel (National Advisory Committee for Aeronautics, 1955), also by Edward A. Fletcher, Melvin Gerstein, Robert G. Dorsch, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Combustion of smoke in diffusion and bunsen flames (National Advisory Committee for Aeronautics, 1951), also by Thomas P. Clark (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Comparison of experimentally and analytically determined windmilling characteristics of a compressor with low over-all pressure ratio (National Advisory Committee for Aeronautics, 1958), also by James E. Hatch, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine (National Advisory Committee for Aeronautics, 1957), also by Cavour H. Hauser, William J. Nusbaum, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Component performance investigation of J71 experimental turbine. [Part] V, Effect of third stage shrouding on internal-flow conditions of J71-97 turbine (National Advisory Committee for Aeronautics, 1956), also by Donald A. Petrash, Elmer H. Davison, Harold J. Schum, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Compressor-blade vibration and performance in a J47-23 turbojet engine under conditions of rotating stall (National Advisory Committee for Aeronautics, 1955), also by Morgan P. Hanson, Andre J. Meyer, Donald F. Johnson, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Compressor-blade vibration of a J57-P-1 turbojet engine during exploratory operation with inlet-pressure distortions (National Advisory Committee for Aeronautics, 1955), also by Morgan P. Hanson and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Conduction and film cooling of leading and trailing edges of rotor blades (National Advisory Committee for Aeronautics, 1951), also by Vernon L. Arne and Jack B. Esgar (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Correlation of physical properties of ceramic materials with resistance to fracture by thermal shock (National Advisory Committee for Aeronautics, 1949), also by W. G. Lidman and A. R. Bobrowsky (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Correlation of turbojet combustor carbon formation with smoke-volatility index, smoke point, and NACA K factor (National Advisory Committee for Aeronautics, 1955), also by Edmund R. Jonash, William P. Cook, Helmut F. Butze, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Correlation of turbulent heat transfer in a tube for the dissociating system N204 <==> 2N02. (National Advisory Committee for Aeronautics, 1958), also by Richard S. Brokaw, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds (National Advisory Committee for Aeronautics, 1956), also by Andrew Beke, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Design and experimental investigation of a single-stage turbine with a rotor entering relative Mach number of 2 (National Advisory Committee for Aeronautics, 1958), also by Thomas P. Moffitt and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Design and experimental performance of standard turbine (National Advisory Committee for Aeronautics, 1957), also by Harold E. Rohlik, Herbert W. Scibbe, William T. Wintucky, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Design, over-all performance and stall characteristics (National Advisory Committee for Aeronautics, 1954), also by George W. Lewis, G. K. Serovy, Francis C. Schwenk, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Determination of aromatics and olefins in wide-boiling petroleum fractions (National Aeronautics and Space Administration, 1950), also by A. E. Spakowski, R. R. Hibbard, A. Evans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Determination of blade-to-coolant heat-transfer coefficients on a forced-convection, water-cooled, single-stage turbine (National Advisory Committee for Aeronautics, 1951), also by John C. Freche and Eugene F. Schum (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Determination of gas-to-blade convection heat-transfer coefficients on a forced-convection, water-cooled single-stage aluminum turbine (National Advisory Committee for Aeronautics, 1951), also by John C. Freche and Eugene F. Schum (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Determination of surge and stall limits of an axial-flow turbojet engine for control applications (National Advisory Committee for Aeronautics, 1953), also by Ross D. Schmidt, Edward W. McGraw, George Vasu, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0 (National Advisory Committee for Aeronautics, 1956), also by Thomas G. Piercy, Bruce G. Chiccine, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Dynamic investigation (National Advisory Committee for Aeronautics, 1949), also by Andre J. Meyer and Howard F. Calvert (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine (National Advisory Committee for Aeronautics, 1956), also by Fred A. Wilcox, Paul Whalen, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of a reduction in stator solidity on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, R. Y. Wong, Warner L. Stewart, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of annular inlet baffles on rotating stall, blade vibration, and performance of an axial-flow compressor in a turbojet engine (National Advisory Committee for Aeronautics, 1955), also by Johnson,Donald F., Morgan P. Hanson, Andre J. Meyer, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), also by Charles F. Zalabak, Arthur N. Curren, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of centerbody boundary-layer removal near the throat of three conical nose inlets at mach 1.6 to 2.0 (National Advisory Committee for Aeronautics, 1955), also by Emil J. Kremzier, George A. Wise, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of circumferential total-pressure gradients typical of single-inlet duct installations on performance of an axial-flow turbojet engine (National Advisory Committee for Aeronautics, 1955), also by S. C. Huntley, Curits L. Walker, Joseph N. Sivo, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades (National Advisory Committee for Aeronautics, 1956), also by Arthur N. Curren, Charles F. Zalabak, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of diffusion processes and temperature on smoking tendencies of laminar diffusion flames (National Advisory Committee for Aeronautics, 1953), also by Rose L. Schalla (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of fuel additives on carbon deposition in a J33 single combustor. [Part] 1, Three metallic-organic additives (National Advisory Committee for Aeronautics, 1952), also by Edmund R. Jonash, William P. Cook, and Jerrold D. Wear (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of fuel drop size and injector configuration on screaming in a 200-pound-thrust rocket engine using liquid oxygen and heptane (National Advisory Committee for Aeronautics, 1958), also by Charles E. Feiler and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of high rotor pressure-surface diffusion on performance of a transonic turbine (National Advisory Committee for Aeronautics, 1955), also by James W. Miser, Daniel E. Monroe, Warner L. Stewart, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of plastic viscosity and yield value on spray characteristics of magnesium-slurry fuel (National Advisory Committee for Aeronautics, 1957), also by George M. Prok and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of pressure on smoking tendency of diffusion flames (National Advisory Committee for Aeronautics, 1953), also by Rose L. Schalla and Glen E. McDonald (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800 degrees R (National Advisory Committee for Aeronautics, 1948), also by Robert C. Kohl and Robert G. Larkin (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of properties of primary fluid on performance of cylindrical shroud ejectors (National Advisory Committee for Aeronautics, 1954), also by Fred D. Kochendorfer (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effect of surface-active additives on physical behavior of 50-percent slurries of 1.5-micron magnesium in n-decane (National Advisory Committee for Aeronautics, 1955), also by Murray L. Pinns (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Effects of special leading- and trailing-edge modifications on blade temperature (National Advisory Committee for Aeronautics, 1951), also by Herman H. Ellerbrock, Gordon T. Smith, and Charles F. Zalabak (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Endurance evaluation of several tube-filled rotor blades (National Advisory Committee for Aeronautics, 1952), also by Jack B. Esgar and John L. Clure (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Endurance evaluation of shell-supported turbine rotor blades made of timken 17-22A (S) steel (National Advisory Committee for Aeronautics, 1951), also by Francis S. Stepka, John L. Clure, and H. Robert Bear (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Engine design-point performance (National Advisory Committee for Aeronautics, 1954), also by James E. Hubbartt, Wilson B. Schramm, and R. J. Rossbach (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Engine performance of overtemperature heat-treated S-816 buckets (National Advisory Committee for Aeronautics, 1956), also by Robert A. Signorelli, F. B. Garrett, John W. Weeton, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Estimation of specific surface of fine divided magnesium (National Advisory Committee for Aeronautics, 1956), also by Murray L. Pinns and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: An evaluation of electropolished and nonelectropolished blades of alloys refractaloy 26, M-252, and waspaloy in a J33-9 turbojet engine (National Advisory Committee for Aeronautics, 1955), also by Francis Jacob Clauss, J. R. Johnston, R. A. Signorelli, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Evaluation of five conical center-body supersonic diffusers at several angles of attack (National Advisory Committee for Aeronautics, 1952), also by Gerald W. Englert and Leonard J. Obery (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Evaluation of the use of electrical resistance for detecting overtemperatured S-816 turbine blades (National Advisory Committee for Aeronautics, 1957), also by Leonard Robins, Lewis A. Rodert, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Examination of smoke and carbon from turbojet-engine combustors (National Advisory Committee for Aeronautics, 1952), also by Thomas P. Clark and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Experimental cooling-air impeller performance and turbine rotor temperatures in modified J33 split-disk rotor up to speeds of 10,000 RPM (National Advisory Committee for Aeronautics, 1952), also by Alfred J. Nachtigall, Robert R. Ziemer, and Charles F. Zalabak (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Experimental investigation at Mach numbers 1.88, 3.16, and 3.83 of pressure drag of wedge diverters simulating boundary-layer-removal systems for side-inlets (National Advisory Committee for Aeronautics, 1954), also by Thomas G. Piercy, Harry W. Johnson, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Experimental investigation of direct control of diffuser pressure on 16-inch ram-jet engine (National Advisory Committee for Aeronautics, 1955), also by William R. Dunbar, Herbert G. Hurrell, George Vasu, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Experimental investigation of external water-spray cooling in a turbojet engine utilizing several injection configurations including orifices in the rotor-blade bases (National Advisory Committee for Aeronautics, 1955), also by Roy A. McKinnon, John C. Freche, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Experimental investigation of free-convection heat transfer in vertical tube at large grashof numbers (National Advisory Committee for Aeronautics, 1952), also by E. R. G. Eckert, A. J. Diagula, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Experimental investigation of the heat-transfer characteristics of an air-cooled sintered porous turbine blade (National Advisory Committee for Aeronautics, 1952), also by Louis J. Schafer, Hadley T. Richards, and Edward R. Bartoo (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Fabrication and endurance of air-cooled strut-supported turbine blades with struts cast of X-40 alloy (National Advisory Committee for Aeronautics, 1956), also by Eugene F. Schum, Robert E. Oldrieve, Francis S. Stepka, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Five organo-metallic additives (National Advisory Committee for Aeronautics, 1955), also by Edmund R. Jonash, William P. Cook, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A flow calorimeter for determining combustion efficiency from residual enthalpy of exhaust gases (National Advisory Committee for Aeronautics, 1954), also by Albert Evans, Robert R. Hibbard, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99. [Part] 2, Isentropic-spike all-external compression inlet (National Advisory Committee for Aeronautics, 1951), also by L. J. Obery, G. W. Englert, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Free fall and evaporation of n-octane droplets in the atmosphere as applied to the jettisoning of aviation gasoline at altitude (National Advisory Committee for Aeronautics, 1953), also by Herman H. Lowell (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Fuel characteristics pertinent to the design of aircraft fuel systems. Supplement 1 - Additional information on MIL-F-7914(AER) Grade JP-5 fuel and several fuel oils (National Advisory Committee for Aeronautics, 1953), also by Henry C. Barnett, Robert R. Hibbard, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Heat of combustion of the product formed by the reaction of diborane and an unsaturated hydrocarbon (LFPL-MZ-2) (National Advisory Committee for Aeronautics, 1953), also by Harrison Allen and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: High-altitude performance of 9.5-inch-diameter tubular experimental combustor with fuel staging (National Advisory Committee for Aeronautics, 1954), also by Wilfred E. Scull (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Ignition-delay characteristics in modified open-cup apparatus of several fuels with nitric acid oxidants within temperature range 70 degrees to 105 degrees F (National Advisory Committee for Aeronautics, 1951), also by Riley O. Miller (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Infiltration of titanium carbide with several metals (National Advisory Committee for Aeronautics, 1952), also by Raymond S. Gurnick and Anthony L. Cooper (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Influence of external variables on smoking of benzene flames (National Advisory Committee for Aeronautics, 1952), also by Thomas P. Clark (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: An inlet design concept to reduce flow distortion at angle of attack (National Advisory Committee for Aeronautics, 1957), also by Carl F. Schueller, Leonard E. Stitt, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics (National Advisory Committee for Aeronautics, 1956), also by H. George Krull, William T. Beale, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Internal performance of several divergent-shroud ejector nozzles with high divergence angles (National Advisory Committee for Aeronautics, 1957), also by Arthur M. Trout, John H. Povolny, S. Stephen Papell, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles (National Advisory Committee for Aeronautics, 1956), also by Donald P. Hearth, Robert W. Cubbison, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination (National Advisory Committee for Aeronautics, 1958), also by J. Cary Nettles, Robert C. Campbell, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades (National Advisory Committee for Aeronautics, 1948), also by John C. Freche, Bob W. Sheflin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of acceleration characteristics of a single-spool turbojet engine (National Advisory Committee for Aeronautics, 1953), also by Frank L. Oppenheimer and George J. Pack (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air (National Advisory Committee for Aeronautics, 1957), also by James F. Connors, Rudolph C. Meyer, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of an underslung half-cone inlet with compression surface mounted outboard from fuselage at mach numbers of 1.5, 1.8, and 2.0 (National Advisory Committee for Aeronautics, 1958), also by Richard A. Yeager, Laurence W. Gertsma, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of axially symmetric and two-dimensional multinozzles for producing supersonic streams (National Advisory Committee for Aeronautics, 1952), also by Eli Reshotko and Rudolph C. Haefeli (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of combustion screech and a method of its control (National Advisory Committee for Aeronautics, 1954), also by James L. Harp, Lively Bryant, and Wallace W. Velie (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of effect of fluoride on corrosion of 2S-0 aluminum and 347 stainless steel in fuming nitric acid a t 170° (National Advisory Committee for Aeronautics, 1954), also by Charles E. Feiler, Gerald Morrell, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of effects of reynolds number on large double-entry centrifugal compressor (National Advisory Committee for Aeronautics, 1952), also by Karl Kovach and Joseph R. Withee (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of shock : boundary-layer interaction on the spike of a conical-spike nose inlet (National Advisory Committee for Aeronautics, 1957), also by George A. Wise, William H. Sterbentz, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes (National Advisory Committee for Aeronautics, 1955), also by Ray E. Budinger, Harold R. Kaufman, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of three types of supersonic diffuser over a range of Mach numbers from 1.75 to 2.74 (National Advisory Committee for Aeronautics, 1951), also by L. Eugene Baughman, Larence I. Gould, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of transonic turbine designed for zero diffusion of suction-surface velocity (National Advisory Committee for Aeronautics, 1954), also by Warren J. Whitney, R. Y. Wong, and Daniel E. Monroe (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5. [Part] I, , Velocity-diagram study (National Advisory Committee for Aeronautics, 1956), also by James W. Miser, Warner L. Stewart, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Low-pressure performance of different diameter experimental combustor liners (National Advisory Committee for Aeronautics, 1954), also by Ralph T. Dittrich and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Low-pressure performance of experimental prevaporizing tubular combustor using approximately stoichiometric admission of fuel-air mixture into the primary zone (National Advisory Committee for Aeronautics, 1954), also by Robert R. Hibbard, Wilfred E. Scull, and Allen J. Metzler (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Lumped reflector parameters for two-group reactor calculations (National Advisory Committee for Aeronautics, 1952), also by Daniel Fieno, Robert B. Spooner, and Harold Schneider (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A method for determining core dimensions of heat exchanger with one dominating film resistance and verification with experimental data (National Advisory Committee for Aeronautics, 1957), also by John N. B. Livingood, Anthony J. Diaguila, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A method for determining turbine design characteristics for rocket turbodrive applications (National Advisory Committee for Aeronautics, 1958), also by Warner L. Stewart, Warren J. Whitney, David G. Evans, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: NACA Conference on Turbine Cooling : a compilation of the papers presented by NACA staff members, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, November 9, 1949 (NACA, 1949), also by Ohio) NACA Conference on Turbine Cooling (1949 : Cleveland and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: NACA Conference on Turbine Materials and Cooling : a compilation of the papers presented, Lewis Flight Propulsion Laboratory, Cleveland, Ohio, March 15, 1951 (NACA, 1951), also by Ohio) NACA Conference on Turbine Materials and Cooling (1951 : Cleveland and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Nine oxygen-bearing compounds (National Advisory Committee for Aeronautics, 1956), also by Edmund R. Jonash, William P. Cook, Jerrold D. Wear, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Note on performance of aircraft ejector nozzles at high secondary flows (National Advisory Committee for Aeronautics, 1954), also by Fred D. Kochendorfer (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Operational characteristics (National Advisory Committee for Aeronautics, 1948), also by William A. Fleming (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Perforated supersonic inlet (National Advisory Committee for Aeronautics, 1948), also by Albert H. Schroeder and James F. Connors (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance and windmilling drag characteristics (National Advisory Committee for Aeronautics, 1948), also by William A. Fleming and Robert O. Dietz (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance comparisons of JFC-2 and MIL-F-5624A (JP-3) fuels in tubular and annular combustors (National Advisory Committee for Aeronautics, 1952), also by Richard J. McCafferty and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance investigation of can-type combustor from British turbojet engine and comparison of this combustor with can-type combustor from U.S. turbojet engine (National Advisory Committee for Aeronautics, 1950), also by William P. Cook and Richard G. Koch (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance of a translating-double-cone axisymmetric inlet with cowl bypass at mach number from 2.0 to 3.5 (National Advisory Committee for Aeronautics, 1957), also by James F. Connors, GeorgeA. Wise, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance of experimental channeled-wall annular turbojet combustor at conditions simulating high-altitude supersonic flight. [Part] I, U-shaped channel walls for secondary-air entry / (National Advisory Committee for Aeronautics, 1955), also by Eugene V. Zettle, Robert Friedman, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0 (National Advisory Committee for Aeronautics, 1957), also by Paul C. Simon, Ronald G. Huff, Dennis W. Brown, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance of pure fuels in a single J33 combustor. [Part] III, Five hydrocarbon gaseous fuels and one oxygenated-hydrocarbon gaseous fuel (National Advisory Committee for Aeronautics, 1956), also by Arthur L. Smith, Jerrold D. Wear, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Performance of supersonic axial-flow compressors based on one-dimensional analysis (National Advisory Committee for Aeronautics, 1949), also by Linwood C. Wright and John F. Klapproth (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Photographic investigation of air-flow patterns in transparent one-sixth sector of annular turbojet-engine combustor with axial-slot-type air admission (National Advisory Committee for Aeronautics, 1954), also by Charles C. Graves and J. Dean Gernon (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Photographic studies of preignition environment and flame initiation in turbojet-engine combustors (National Advisory Committee for Aeronautics, 1953), also by David M. Straight and J. Dean Gernon (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preliminary attempts at isothermal compression of a supersonic air stream (National Advisory Committee for Aeronautics, 1956), also by E. Perchonok, F. Wilcox, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preliminary engine investigation (National Advisory Committee for Aeronautics, 1949), also by Andre J. Meyer and Howard F. Calvert (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preliminary investigation of a perforated axially symmetric nozzle for varying nozzle pressure ratios (National Advisory Committee for Aeronautics, 1953), also by Eli Reshotko (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preliminary investigation of hollow-bladed turbines having closed and open blade tips (National Advisory Committee for Aeronautics, 1955), also by Gordon T. Smith, Robert O. Hickel, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet (National Advisory Committee for Aeronautics, 1957), also by Milton A. Beheim, Thomas G. Piercy, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preliminary investigation of the strength and endurance of plastic-impregnated fiberglass compressor blades (National Advisory Committee for Aeronautics, 1955), also by Donald F. Johnson and Andre J. Meyer (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preliminary studies of rolling-contact fatigue life of high-temperature bearing materials (National Advisory Committee for Aeronautics, 1958), also by Thomas L. Carter, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preparation and handling of magnesium-hydrocarbon slurries for jet-engine applications (National Advisory Committee for Aeronautics, 1955), also by Henry C. Barnett, Paul H. Wise, Albert M. Lord, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preparation and properties of concentrated boron-hydrocarbon slurry fuels (National Advisory Committee for Aeronautics, 1954), also by Irving A. Goodman and Virginia O. Fenn (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preparation of 50 percent boron-hydrocarbon slurries using combinations of glycerol sorbitan laurate with various thickeners (National Advisory Committee for Aeronautics, 1955), also by Irving A. Goodman, Virginia O. Fenn, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Preparation of dipentaborylmethane by Friedel-Crafts reaction (National Advisory Committee for Aeronautics, 1958), also by Albert C. Antoine, United States. National Adviosry Committee for Aeronautics, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: The rate of decomposition of liquid pentaborane from 85⁰ to 202⁰ C (National Advisory Committee for Aeronautics, 1955), also by Glen E. McDonald and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Relation of turbine-engine combustion efficiency to second-order reaction kinetics and fundamental flame speed (National Advisory Committee for Aeronautics, 1954), also by J. Howard Childs and Charles C. Graves (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Review of the toxicological properties of pentaborane, diborane, decaborane, and boric acid (National Advisory Committee for Aeronautics, 1956), also by Joseph M. Lamberti and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Rotating stall investigation of the 0.72 hub-tip ratio single-stage compressor (National Advisory Committee for Aeronautics, 1954), also by Robert W. Graham, Vasily D. Prian, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Rotor blades with 34 steel tubes in cooling-air passages (National Advisory Committee for Aeronautics, 1950), also by Robert O. Hickel and Gordon T. Smith (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Rotor blades with split trailing edges (National Advisory Committee for Aeronautics, 1951), also by Gordon T. Smith and Robert O. Hickel (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Self-ignition temperatures and flash points of some high-energy fuels (National Advisory Committee for Aeronautics, 1957), also by Barbara Pusanski and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Seven commercial organo-metallic additives (National Advisory Committee for Aeronautics, 1954), also by Vincent F. Hlavin and William P. Cook (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Simulated afterburner performance with hydrogen peroxide injection for thrust augmentation (National Advisory Committee for Aeronautics, 1956), also by Allen J. Metzler, Jack S. Grobman, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Simulated altitude performance of two annular combustors with continuous axial openings for admission of primary air (National Advisory Committee for Aeronautics, 1950), also by Eugene V. Zettle and Herman Mark (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Some effects of blade trailing-edge thickness on performance of a single-stage axial-flow compressor (National Advisory Committee for Aeronautics, 1951), also by J. J. Moses and G. K. Serovy (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Spontaneous ignition limits of pentaborane (National Advisory Committee for Aeronautics, 1957), also by Rose L. Schalla and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Spontaneous ignition of pentaborane sprays in a hot-air stream (National Advisory Committee for Aeronautics, 1956), also by Erwin A. Lezberg, Albert M. Lord, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid (National Advisory Committee for Aeronautics, 1950), also by Gerald Morrell, Jack C. Humphrey, John L. Sloop, and Dezso J. Ladanyi (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Static investigation of several jet deflectors for longitudinal control of an aircraft (National Advisory Committee for Aeronautics, 1955), also by Alfred S. Valerino (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine (National Advisory Committee for Aeronautics, 1955), also by Reeves P. Cochran, Robert P. Dengler, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A study of liquid boric oxide particle growth rates in a gas stream from a simulated jet engine combustor (National Advisory Committee for Aeronautics, 1957), also by Paul C. Setze, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A summary of design information for water-cooled turbines (National Advisory Committee for Aeronautics, 1951), also by John C. Freche (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A summary of preliminary investigations into the characteristics of combustion screech on ducted burners (National Advisory Committee for Aeronautics, 1954), also by Lewis Laboratory Staff and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Survey of hydrogen combustion properties (National Advisory Committee for Aeronautics, 1957), also by Isadore L. Drell, Frank E. Belles, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A survey of methods for turbojet thrust measurement applicable to flight installation (National Advisory Committee for Aeronautics, 1955), also by William A. Fleming, David S. Gabriel, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A temperature-schedule acceleration control for a turbojet engine and its use with a speed control (National Advisory Committee for Aeronautics, 1957), also by Theodore F. Gerus, Herbert J. Heppler, Albert G. Powers, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas (National Advisory Committee for Aeronautics, 1957), also by Charles C. Graves, Jack S. Grobman, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant. [Part] I, Frozen composition (National Advisory Committee for Aeronautics, 1956), also by Sanford Gordon, Vearl N. Huff, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines. [Part] 3, Liquid ammonia (National Advisory Committee for Aeronautics, 1952), also by Vearl N. Huff and Sanford Gordon (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines. [Part] 2, Hydrazine (National Advisory Committee for Aeronautics, 1952), also by Vearl N. Huff and Sanford Gordon (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition (National Advisory Committee for Aeronautics, 1957), also by Sanford Gordon, Kenneth S. Drellishak, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles (National Advisory Committee for Aeronautics, 1955), also by Richard J. McCafferty, Richard H. Donlon, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Transient operating characteristics of a turbojet engine when subjected to step changes in fuel flow (National Advisory Committee for Aeronautics, 1950), also by Arthur H. Bell and J. Elmo Farmer (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: True airspeed measurement by ionization-tracer technique (National Advisory Committee for Aeronautics, 1952), also by Bemrose Boyd, George H. Brodie, Robert G. Dorsch, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation (National Advisory Committee for Aeronautics, 1956), also by Allen J. Metzler, Jack S. Grobman, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Vapor-fuel-distribution effects on combustion performance of a single tubular combustor (National Advisory Committee for Aeronautics, 1950), also by Richard J. McCafferty (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05 (National Advisory Committee for Aeronautics, 1956), also by James F. Connors, Rudolph C. Meyer, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Variation in smoking tendency among low molecular weight hydrocarbons (National Advisory Committee for Aeronautics, 1952), also by Rose L. Schalla and Glen E. McDonald (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Visual study of free convection in a narrow vertical enclosure (National Advisory Committee for Aeronautics, 1956), also by E. M. Sparrow, Samuel J. Kaufman, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Visualization of secondary-flow phenomena in blade row (National Advisory Committee for Aeronautics, 1952), also by H. Z. Herzig, G. R. Costello, and A. G. Hansen (page images at HathiTrust)
• Lewis Flight Propulsion Laboratory: Wing tip with subsonic trailing edge (National Advisory Committee for Aeronautics, 1949), also by Harold Mirels and James M. Jagger (page images at HathiTrust)

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