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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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
Theoretical Determination of Low-drag Supercavitating Hydrofoils and Their Two-dimensional Characteristics at Zero Cavitation... Theoretical Determination of Low-drag Supercavitating Hydrofoils and Their Two-dimensional Characteristics at Zero Cavitation Number (Paperback)
Langley Aeronautical Laboratory
R342 Discovery Miles 3 420 Ships in 10 - 15 working days
Correlation of Supersonic Convective Heat-transfer Coefficients From Measurements of the Skin Temperature of a Parabolic Body... Correlation of Supersonic Convective Heat-transfer Coefficients From Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10) (Paperback)
Langley Aeronautical Laboratory
R344 Discovery Miles 3 440 Ships in 10 - 15 working days
Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating Near the Free Water... Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating Near the Free Water Surface (Paperback)
Langley Aeronautical Laboratory
R456 Discovery Miles 4 560 Ships in 10 - 15 working days
Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence... Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel (Hardcover)
Langley Aeronautical Laboratory
R678 Discovery Miles 6 780 Ships in 10 - 15 working days
Flight Investigation at High Speeds of Flow Conditions Over an Airplane Wing as Indicated by Surface Tufts (Paperback): Langley... Flight Investigation at High Speeds of Flow Conditions Over an Airplane Wing as Indicated by Surface Tufts (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390 Ships in 10 - 15 working days
Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012... Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012 Airfoil With Various Types of Aileron (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
Flow of Gas Through Turbine Lattices (Paperback): Langley Aeronautical Laboratory Flow of Gas Through Turbine Lattices (Paperback)
Langley Aeronautical Laboratory
R468 Discovery Miles 4 680 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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 Ships in 10 - 15 working days
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