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258 Matching Results

Start Over Resource Type Report Year 1941

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Results: 1 - 24 of 258 next
Best Match Title Creator Date Created (Newest) Date Created (Oldest) Date Added (Newest) Date Added (Oldest)
Comparison of Vee-Type and Conventional Tail Surfaces in Combination with Fuselage and Wing in the Variable-Density Tunnel
Comparison of Vee-Type and Conventional Tail Surfaces in Combination with Fuselage and Wing in the Variable-Density Tunnel
The Calculation of Span Load Distributions of Swept-Back Wings
The Calculation of Span Load Distributions of Swept-Back Wings
Methods of Analyzing Wind-Tunnel Data for Dynamic Flight Conditions
Methods of Analyzing Wind-Tunnel Data for Dynamic Flight Conditions
Supplement to Comparison of Automatic Control Systems
Supplement to Comparison of Automatic Control Systems
Effects of Some Present-Day Airplane Design Trends on Requirements for Lateral Stability
Effects of Some Present-Day Airplane Design Trends on Requirements for Lateral Stability
Design of Nozzles for the Individual Cylinder Exhaust Jet Propulsion System
Design of Nozzles for the Individual Cylinder Exhaust Jet Propulsion System
Spin Tests of Two Models of a Low-Wing Monoplane to Investigate Scale Effect in the Model Test Range
Spin Tests of Two Models of a Low-Wing Monoplane to Investigate Scale Effect in the Model Test Range
Use of Brine in a Kansas Field for Secondary Recovery of Oil
Use of Brine in a Kansas Field for Secondary Recovery of Oil
Petroleum Engineering Study of the Anahuac Field, Chambers County, Texas
Petroleum Engineering Study of the Anahuac Field, Chambers County, Texas
Annual Report of the Mining Division, Fiscal Year 1941
Annual Report of the Mining Division, Fiscal Year 1941
United States Earthquakes 1939
United States Earthquakes 1939
United States Earthquakes 1941
United States Earthquakes 1941
Magnetic Separation of Ores
Magnetic Separation of Ores
The Precipitation of Uranium Peroxide in the Presence of Fluorides
The Precipitation of Uranium Peroxide in the Presence of Fluorides
Past Lode-Gold Production from Alaska
Past Lode-Gold Production from Alaska
Some Quicksilver Prospects in Adjacent Parts of Nevada, California, and Oregon
Some Quicksilver Prospects in Adjacent Parts of Nevada, California, and Oregon
Chemical Properties of Uranium Hexafluoride, UF6
Chemical Properties of Uranium Hexafluoride, UF6
A New Crystalline Hydrate of Uranium Tetrafluoride, 2UF$sub 4$/center dot/ 5H$sub 2$O, and Its Dehydration to Anhydrous Uranium Tetrafluoride
A New Crystalline Hydrate of Uranium Tetrafluoride, 2UF$sub 4$/center dot/ 5H$sub 2$O, and Its Dehydration to Anhydrous Uranium Tetrafluoride
Pressure-Distribution Measurements of a Low-Drag Airfoil With Slotted Flap Submitted by Curtiss-Wright Corporation
Pressure-Distribution Measurements of a Low-Drag Airfoil With Slotted Flap Submitted by Curtiss-Wright Corporation
Wind-Tunnel Investigation of Control-Surface Characteristics 3: A Small Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
Wind-Tunnel Investigation of Control-Surface Characteristics 3: A Small Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
Wind-Tunnel Investigation of Control-Surface Characteristics 4: A Medium Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
Wind-Tunnel Investigation of Control-Surface Characteristics 4: A Medium Aerodynamic Balance of Various Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0009 Airfoil
Wind-tunnel investigation of control-surface characteristics II : a large aerodynamic balance of various nose shapes with a 30-percent-chord flap on an NACA 0009 airfoil
Wind-tunnel investigation of control-surface characteristics II : a large aerodynamic balance of various nose shapes with a 30-percent-chord flap on an NACA 0009 airfoil
Wind-tunnel investigation of control-surface characteristics 1: effect of gap on the aerodynamic characteristics of an NACA 0009 airfoil with a 30-percent-chord plain flap
Wind-tunnel investigation of control-surface characteristics 1: effect of gap on the aerodynamic characteristics of an NACA 0009 airfoil with a 30-percent-chord plain flap
Wind-tunnel investigation of an NACA 23012 airfoil with a 30 percent chord Maxwell slate and with trailing-edge flaps
Wind-tunnel investigation of an NACA 23012 airfoil with a 30 percent chord Maxwell slate and with trailing-edge flaps