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JPSL Elevation Drawing (1952)
AERL Wartime Research Authorizations (1943)
General H.H. Arnold Speech to AERL Employees (1944)
Place of NACA in U.S. Aviation (1943)
Model Research: National Advisory Committee for Aeronautics 1915-1958
Review and status of liquid-cooling technology for gas turbines
Afterburner Story (1954)
Turbojet Revolution at Lewis Research Center (1984)
The Development of the Whittle Turbojet (1997)
Analytical and Experimental Investigation of Thrust Augmentation of Axial- and Centrifugal-compressor Turbojet Engines by Injection of Water and Alcohol in Combustion Chambers
Fuel tests on an I-16 jet-propulsion engine at static sea-level conditions
Experimental Investigation of Thrust Augmentation of a Turbojet Engine at Zero Ram by Means of Tail-pipe Burning
Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by injection of water and alcohol at compressor inlets
Experimental Investigation of Thrust Augmentation of Axial-flow-type 4000-pound-thrust Turbojet Engine by Water and Alcohol Injection at Compressor Inlet
Investigation of Thrust Augmentation of a 1600-pound Thrust Centrifugal-flow-type Turbojet Engine by Injection of Refrigerants at Compressor Inlets
Investigation of Several Clamshell Variable-area Exhaust Nozzles for Turbojet Engines
Experimental Investigation of Thrust Augmentation of 4000-pound-thrust Axial-flow-type Turbojet Engine by Interstage Injection of Water-alcohol Mixtures in Compressor
Experimental Investigation of Thrust Augmentation of 4000-pound-thrust Centrifugal-flow-type Turbojet Engine by Bleedoff
Experimental Investigation of Turbojet-engine Thrust Augmentation by Combined Compressor Coolant Injection and Tail-pipe Burning
Experimental Sea-level Static Investigation of a Short Afterburner
An Evaluation of Turbojet Engine Thrust Control by Exhaust-nozzle-area Modulation and Compressor-inlet Throttling
Afterburner performance with combustion-chamber lengths from 10 to 62 inches at several afterburner-inlet temperatures
Investigation of Thrust Augmentation Using Water-alcohol Injection on a 5200-pound-thrust Axial-flow-type Turbojet Engine at Static Sea-level Conditions
Investigation of Sea-Level Performance of I-16 Turbojet Engine at Zero Ram with XFR-1 Intake Duct Shroud, and Tail Pipe
Performance of Short Annular Diffusers for Afterburners (1954)
Tests of an Adjustable-area Exhaust Nozzle for Jet-propulsion Engines
Low-Pressure-Loss Short Afterburner for Thrust Augmentation (1955)
Experimental Investigation of Cermet Turbine Blades in an Axial-flow Turbojet Engine
Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine
Experimental Investigation of Effect of Cooling Air on Turbine Performance of Two Turbojet Engines Modified for Air-cooling
Preliminary Investigation of Several Root Designs for Cermet Turbine Blades in Turbojet Engine III : Curved-root Design
Investigation of Turbojet Engine Performance at Speeds and Gas Temperatures Above Rated Using Turbine-blade External Water-spray Cooling from Stationary Injection Orifices
Experimental Investigation of an Air-Cooled Turbine Operating in a Turbojet Engine at Turbine Inlet Temperatures up to 2500 F
Preliminary Investigation of Several Root Designs for Cermet Turbine Blades in Turbojet Engine II : Root Design Alterations
Turbine cooling - Its limitations and its future
NACA Conference on Turbojet-Engine Thrust Augmentation Research: A Compilation of the Papers Presented by NACA Staff Members
Summary of NACA Research on Afterburners for Turbojet Engines
Fuels Research Talk at NACA Inspection (1947)
Full-Scale Turbojet Engine Research Inspection Talk (1948)
Turbine Research Inspection Talk (1949)
Turbine Research Inspection Talk (1947)
Investigation of characteristics of pressure waves generated in water filled tanks impacted by high-velocity projectiles
Accelerated cavitation damage of steels and superalloys in liquid metals
Effect of projectile size and material on impact fracture of walls of liquid-filled tanks
Cavitation damage of stainless steel, nickel, and an aluminum alloy in water for ASTM round robin tests
Effect of ultrasonic vibration on precipitation hardening of steels and superalloys
Effect of temperature and pressure on cavitation damage to a cobalt base alloy in sodium
Experimental performance characteristics of three identical Brayton rotating units
A review of NASA research to determine the resistance of materials to cavitation damage in liquid metal environments
Meteoroid damage assessment - Space vehicle design criteria
Performance of a Brayton power system with a space type radiator
A Historical Review of Brayton and Stirling Power Conversion Technologies for Space Applications
Catastrophic Fracturing of Tanks when Impacted by Projectiles (1964)
Space Debris Hazard Evaluation
Concepts for cost reduction on turbine engines for general aviation
Experience with low cost jet engines
Experimental test results of a generalized parameter fuel control
Small, low-cost, expendable turbojet engine. 1: Design, fabrication, and preliminary testing
Small, low cost, expendable turbojet engine. 2: Performance characteristics
Infrared suppressor effect on T63 turboshaft engine performance
Test evaluation of a laminated wood wind turbine blade concept
Examination, evaluation and repair of laminated wood blades after service on the Mod-OA wind turbine
Exhaust Nozzles for Propulsion Systems with Emphasis on Supersonic Cruise Aircraft
Structural properties of laminated Douglas fir/epoxy composite material
Wind Turbine Wood-Epoxy Blade Test (1978)
Comparison of experimental and predicted heat transfer characteristics for a cylindrical ejector
Oxidation and thermal fatigue cracking of nickel- and cobalt-base alloys in a high velocity gas stream
Hot-salt stress-corrosion of a titanium alloy under a simulated turbine-engine compressor environment
Furnace and high-velocity oxidation of aluminide-coated cobalt super-alloy WI-52
Cyclic furnace oxidation of clad WI-52 systems at 1040 C and 1090 C
Cyclic oxidation evaluation: Approaching application conditions
High gas velocity oxidation and hot corrosion testing of oxide dispersion-strengthened nickel-base alloys
Two-layer thermal barrier coating for turbine airfoils - furnace and burner rig test results
High Velocity Burner Rig Oxidation and Thermal Fatigue Behavior of Si3N4- and SiC Base Ceramics to 1370 Deg C
Analysis of the response of a thermal barrier coating to sodium and vanadium doped combustion gases
Evaluation of hot corrosion behavior of thermal barrier coatings
Replaceable blade turbine and stationary specimen corrosion testing facility
NASA Lewis Research Center lean-, rich-burn materials test burner rig
Hot Corrosion Test Facility at the NASA Lewis Special Projects Laboratory
Thermal Conductivity and Elastic Modulus Evolution of Thermal Barrier Coatings under High Heat Flux Conditions
SiC and Si3N4 Recession Due to SiO2 Scale Volatility Under Combustor Conditions
SiC/SiC Leading Edge Turbine Airfoil Tested Under Simulated Gas Turbine Conditions
NASA GRC's High Pressure Burner Rig Facility and Materials Test Capabilities
Development of Advanced Thermal and Environmental Barrier Coatings Using a High-Heat-Flux Testing Approach
A High Temperature Cyclic Oxidation Data Base for Selected Materials Tested at NASA Glenn Research Center
Thermal Conductivity of Advanced Ceramic Thermal Barrier Coatings Determined by a Steady-state Laser Heat-flux Approach
Life Modeling of Thermal Barrier Coatings for Aircraft Gas Turbine Engines
Enabling propulsion materials for high-speed civil transport engines
Cyclic Oxidation Testing and Modelling: A NASA Lewis Perspective
History of Thermal Barrier Coatings for Gas Turbine Engines: Emphasizing NASA's Role from 1942 to 1990
Revisiting the Birth of 7YSZ Thermal Barrier Coatings: Steve Stecura
Turbine Engine Hot Section Technology (HOST)
20171023 131017
B24-in-2017-high-bay-south-end
B24-main-doorway-in-2017
GRC-1945-C-11086
GRC-1945-C-12097b
GRC-1975-C-01427
GRC-2017-C-04843b
IMG 4098
JPSL-addition-C14c
JPSL-addition-C18b
SPL-Air-Compressor-2017
SPL-bike-on-porch-color
SPL-Exterior-2017
GRC-2017-C-04986
GRC-1975-C-01420
GRC-1945-C-10732
GRC-1946-C-14300
GRC-1948-C-21302
GRC-1948-C-21846
GRC-1948-C-21848
GRC-1948-C-21849
GRC-1954-C-35146
GRC-1955-C-38783
GRC-1960-C-54527
GRC-1971-C-01068
GRC-1972-C-02814
GRC-1975-C-01415
GRC-1975-C-01422
GRC-1975-C-01429
GRC-1975-C-01434
GRC-1991-C-06954
GRC-2017-C-04662
GRC-2017-C-04663
GRC-2017-C-04971
GRC-2017-C-04995
GRC-2017-C-09684
GRC-1975-C-01417
GRC-2006-C-01464
GRC-1950-C-26287
GRC-1991-C-06946
GRC-1975-C-01430
GRC-1976-C-00439
GRC-1944-C-05064
GRC-1945-C-12097
GRC-1948-C-21925
GRC-1952-C-30939
GRC-1960-C-53352
GRC-1960-C-53919b
GRC-1964-C-67770
GRC-1964-C-72684
GRC-1975-C-01420
GRC-1975-C-01433
GRC-1979-C-00503
GRC-1989-C-14139
GRC-1991-C-02311
GRC-2008-C-04178
GRC-2008-C-04179
GRC-2008-C-04180
GRC-2017-C-04665
GRC-2017-C-04824
GRC-2017-C-04966
GRC-2017-C-09670
JPSL-addition-C15
GRC-1967-C-02001
GRC-1971-C-01067
GRC-1972-C-00328
GRC-1972-C-02815
GRC-1978-C-01318
GRC-1979-C-02389
GRC-1980-C-04462
GRC-1986-C-01809
GRC-1988-C-00209
GRC-1993-C-04124
GRC-2017-C-09690
nasa-work-area-005
GRC-1992-C-06665
GRC-1992-C-06666
GRC-1981-C-03553
GRC-1991-C-06953
GRC-1982-C-02515
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GRC-1966-C-03884
GRC-1967-C-02156
GRC-1967-C-02157
GRC-1967-C-04472
GRC-1969-C-02625
GRC-1971-C-04318
GRC-1973-C-01682
GRC-1976-C-03743
GRC-1977-C-04251
GRC-1978-C-01376
GRC-1982-C-02320
GRC-1973-C-01177
GRC-1983-C-00820
GRC-1981-C-02122
GRC-1980-C-04074
GRC-1978-C-04959
C-1948-21062
EC98-44817-2-1
GRC-1945-C-10730
GRC-1946-C-14506
GRC-1946-C-15497
GRC-1946-C-15498
GRC-1946-C-15567
GRC-1946-C-15676
GRC-1946-C-15677
GRC-1946-C-17348
GRC-1948-C-20863
GRC-1948-C-22347
GRC-1948-C-22553
GRC-1952-C-30953
GRC-1955-C-37767
NACA-RM-E-6J21-fig3-1
NACA-RM-E9B02-fig4
NACA-RM-E50D17-fig3-1
NACA-RM-E54B09-fig2
GRC-1951-C-28857
GRC-1946-C-16003x
GRC-1946-C-16005x
GRC-1964-C-70106
GRC-1967-C-03726
GRC-1968-C-02409
GRC-1969-C-00405
GRC-1969-C-00441
GRC-1969-C-02598
GRC-1969-C-03698
GRC-1962-C-59287
GRC-1961-C-58380
GRC-1962-C-59004
GRC-1960-C-54526
GRC-1963-C-64255
C1948-22344b
C1951-28436
GRC-1946-C-14508
GRC-1948-C-22763
GRC-1950-C-26891
GRC-1953-C-33274
GRC-1953-C-33276
NACA-RM-E53G02-fig-2
NACA-RM-E54G30-fig2
NACA-RM-E55J04-fig-4
GRC-1950-C-26889
GRC-1955-C-39671
1944-05940
1996-253-7133-011-1
EL-1999-00267
EL-2000-00364
GPN-2000-001571
GRC-1943-C-01251
GRC-1944-C-04825
GRC-1944-C-05060
GRC-1944-C-07495
GRC-1945-C-13064c
GRC-1945-C-13889
GRC-1946-C-15352
GRC-1947-C-19786
GRC-1947-C-19832b
NACA-RM-E7G24-fig-6-1
NACA-RM-No-E7B01-fig2
GRC-1945-C-11086
Alpha-gamma angular correlations in the reaction carbon 12/alpha, alpha prime gamma/ 4.433 MeV/
Alpha-gamma angular correlations in the reaction tin-120/alpha, alpha prime gamma sub 1.18MeV/
Alpha-gamma angular correlations in the reaction nickel-58/alpha, alpha prime gamma sub 1.452MeV/
Elastic and inelastic scattering of 42-MeV alpha particles from even tellurium isotopes
Core excitation in silver, indium, and antimony resulting from inelastic scattering of 42-MeV /6.7-pj/ alpha particles
Scattering of 42-MeV /6.7-pJ/ alpha particles from even isotopes of cadmium
Excited states of barium 136 and barium 134
Excited states of cerium 138 and praseodymium 138 populated by beta decay
Scattering of 42 MeV alpha particles from copper-65
Radiation damage to cadmium sulfide solar cells
A comparison of solar cell damage by alpha particles and protons
Performance and temperature dependencies of proton irradiated n/p GaAs and n/p silicon cells
Potential for use of indium phosphide solar cells in the space radiation environment
Study of the odd strontium isotopes with stripping and pickup reactions
I 123 production for use in nuclear medicine by spallation of xenon
Cyclotron production of I-123: An evaluation of the nuclear reactions which produce this isotope
A target design for irradiation of NaI at high beam current
Self-vapor cooled targets for production of I-123 at high current accelerators
Generation of a plasma in a magnetic mirror geometry
Evaluation of two direct-current methods of plasma production for use in magnetic mirror experiments
Polarization in He sup 3 He sup 4 scattering near 26 MeV
Interaction of 42-MeV alpha particles with helium-3
The p-p and p-t final state interactions in the reaction He-3/d,tp/p
Study of the /alpha,t/ reaction on zirconium-90, molybdenum-92, and molybdenum-96 at 41.5 MeV
Investigation of the /d,alpha/ reaction on aluminum 27
Bids Received for Cyclotron (1948)
Cyclotron Performance Test Results (1955)
External Focusing Equipment Specs (1956)
Possible Utilization of the Cyclotron (1955)
Cyclotron Conversion overview (1966)
Cyclotron Redesign Proposal (1965)
Cyclotron Redesign Request (1965)
Cyclotron Upgrade Contracts (1968)
Cyclotron Milestones (1957-80)
Cyclotron Transfer to Clinic (1981)
Lewis-Clinic Cyclotron Program release (1977)
Neutron Therapy Program articles (1977-91)
NASA-Clinic Cyclotron Agreement (1977)
Description of Materials and Stresses Building (1957)
Materials and Stresses Articles (1948-98)
Materials and Stresses Building Floor Plans (1956)
Photos of M&S Building Construction (1949)
Building 140 Drawings
Cyclotron Beam Modifications (1974)
Cyclotron Floor Plans (1978-81)
Cyclotron Specifications (1947)
Cyclotron Safety Manual (1981)
Neutron Therapy Facility Procedures (1970s)
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