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Showing 1 - 25 of 123 matches in All Departments

Effect of Compressibility on the Hovering Performance of Two 10-foot-diameter Helicopter Rotors Tested in the Langley... Effect of Compressibility on the Hovering Performance of Two 10-foot-diameter Helicopter Rotors Tested in the Langley Full-scale Tunnel (Paperback)
Langley Aeronautical Laboratory
R346 Discovery Miles 3 460
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Ships in 10 - 15 working days
Comparison Between Calculated and Measured Loads on Wing and Horizontal Tail in Pull-up Maneuvers (Paperback): Langley... Comparison Between Calculated and Measured Loads on Wing and Horizontal Tail in Pull-up Maneuvers (Paperback)
Langley Aeronautical Laboratory
R340 Discovery Miles 3 400
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Stresses Around Rectangular Cut-outs in Skin-stringer Panels Under Axial Loads - II (Paperback): Langley Aeronautical Laboratory Stresses Around Rectangular Cut-outs in Skin-stringer Panels Under Axial Loads - II (Paperback)
Langley Aeronautical Laboratory
R460 Discovery Miles 4 600
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Method for Studying the Hunting Oscillations of an Airplane With a Simple Type of Automatic Control (Paperback): Langley... Method for Studying the Hunting Oscillations of an Airplane With a Simple Type of Automatic Control (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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Investigation of Effect of Sideslip on Lateral Stability Characteristics. - III, Rectangular Low Wing on Circular Fuselage With... Investigation of Effect of Sideslip on Lateral Stability Characteristics. - III, Rectangular Low Wing on Circular Fuselage With Variations in Vertical-tail Area and Fuselage Length With and Without Horizontal Tail Surface (Paperback)
Langley Aeronautical Laboratory
R397 Discovery Miles 3 970
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Flight Measurements of the Rudder Control and Sideslip Characteristics of Four Vertical Tail Arrangements on the P-40 Series... Flight Measurements of the Rudder Control and Sideslip Characteristics of Four Vertical Tail Arrangements on the P-40 Series Airplanes (Paperback)
Langley Aeronautical Laboratory
R346 Discovery Miles 3 460
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Electromagnetic-analogy Method of Solving Lifting-surface-theory Problems (Paperback): Langley Aeronautical Laboratory Electromagnetic-analogy Method of Solving Lifting-surface-theory Problems (Paperback)
Langley Aeronautical Laboratory
R345 Discovery Miles 3 450
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Charts for the Determination of Wing Torsional Stiffness Required for Specified Rolling Characteristics or Aileron Reversal... Charts for the Determination of Wing Torsional Stiffness Required for Specified Rolling Characteristics or Aileron Reversal Speed (Paperback)
Langley Aeronautical Laboratory
R345 Discovery Miles 3 450
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Field of Flow About a Jet and Effect of Jets on Stability of Jet-propelled Airplanes (Paperback): Langley Aeronautical... Field of Flow About a Jet and Effect of Jets on Stability of Jet-propelled Airplanes (Paperback)
Langley Aeronautical Laboratory
R395 Discovery Miles 3 950
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Effects of Heat-capacity Lag in Gas Dynamics (Paperback): Langley Aeronautical Laboratory Effects of Heat-capacity Lag in Gas Dynamics (Paperback)
Langley Aeronautical Laboratory
R395 Discovery Miles 3 950
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Climb and High-speed Tests of a Curtiss No. 714-1C2-12 Four-blade Propeller on the Republic P-47C Airplane (Paperback): Langley... Climb and High-speed Tests of a Curtiss No. 714-1C2-12 Four-blade Propeller on the Republic P-47C Airplane (Paperback)
Langley Aeronautical Laboratory
R395 Discovery Miles 3 950
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Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as... Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-flight Tunnel (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-foot-span Fighter-type... Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-foot-span Fighter-type Wing of NACA 230-series Airfoil Sections (Paperback)
Langley Aeronautical Laboratory
R345 Discovery Miles 3 450
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Resistance Tests of Models of Three Flying-boat Hulls With a Length-beam Ration of 10.5 (Paperback): Langley Aeronautical... Resistance Tests of Models of Three Flying-boat Hulls With a Length-beam Ration of 10.5 (Paperback)
Langley Aeronautical Laboratory
R346 Discovery Miles 3 460
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Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic... Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations (Paperback)
Langley Aeronautical Laboratory
R342 Discovery Miles 3 420
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Wind-tunnel Investigation of Aileron Effectiveness of 0.20-airfoil-chord Plain Ailerons of True Airfoil Contour on NACA... Wind-tunnel Investigation of Aileron Effectiveness of 0.20-airfoil-chord Plain Ailerons of True Airfoil Contour on NACA 652-415, 653-418 and 654-421 Airfoil Sections (Paperback)
Langley Aeronautical Laboratory
R340 Discovery Miles 3 400
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Approximate Method for Estimating the Incompressible Laminar Boundary-layer Characteristics on a Flat Plate in Slipping Flow... Approximate Method for Estimating the Incompressible Laminar Boundary-layer Characteristics on a Flat Plate in Slipping Flow (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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Maximum Rates of Control Motion Obtained From Ground Tests (Paperback): Langley Aeronautical Laboratory Maximum Rates of Control Motion Obtained From Ground Tests (Paperback)
Langley Aeronautical Laboratory
R338 Discovery Miles 3 380
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Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds (Paperback): Langley... Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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Effect of Elevator-profile Modifications and Trailing-edge Strips on Elevator Hinge-moment and Other Aerodynamic... Effect of Elevator-profile Modifications and Trailing-edge Strips on Elevator Hinge-moment and Other Aerodynamic Characteristics of a Full-scale Horizontal Tail Surface (Paperback)
Langley Aeronautical Laboratory
R397 Discovery Miles 3 970
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Considerations of Wake-excited Vibratory Stress in a Pusher Propeller (Paperback): Langley Aeronautical Laboratory Considerations of Wake-excited Vibratory Stress in a Pusher Propeller (Paperback)
Langley Aeronautical Laboratory
R340 Discovery Miles 3 400
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Scale-effect Tests in a Turbulent Tunnel of the NACA 653-418, a = 1.0 Airfoil Section With 0.20-airfoil-chord Split Flap... Scale-effect Tests in a Turbulent Tunnel of the NACA 653-418, a = 1.0 Airfoil Section With 0.20-airfoil-chord Split Flap (Paperback)
Langley Aeronautical Laboratory
R341 Discovery Miles 3 410
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Determination of Induced Velocity in Front of an Inclined Propeller by a Magnetic-analogy Method (Paperback): Langley... Determination of Induced Velocity in Front of an Inclined Propeller by a Magnetic-analogy Method (Paperback)
Langley Aeronautical Laboratory
R400 Discovery Miles 4 000
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Development of Cowling for Long-nose Air-cooled Engine in the NACA Full-scale Wind Tunnel (Paperback): Langley Aeronautical... Development of Cowling for Long-nose Air-cooled Engine in the NACA Full-scale Wind Tunnel (Paperback)
Langley Aeronautical Laboratory
R342 Discovery Miles 3 420
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Extended Tables of Stiffness and Carry-over Factor for Structural Members Under Axial Load (Paperback): Langley Aeronautical... Extended Tables of Stiffness and Carry-over Factor for Structural Members Under Axial Load (Paperback)
Langley Aeronautical Laboratory
R340 Discovery Miles 3 400
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