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  3. 1 Health, relationships and personal development  Mind, body and spirit  Psychic powers and phenomena

Psychic powers and phenomena Books

We found 51 Books for langley

ZEN THIS AND THAT RAINBOW ZEN By RaL Edition 2: Wake up to your Self! A Handbook for Humans

ZEN THIS AND THAT RAINBOW ZEN By RaL Edition 2: Wake up to your Self! A Handbook for Humans

Langley, Ray
Createspace, Paperback, New

€ 26,22
Flight Investigation of Internally Balanced Sealed Ailerons in the Presence of a Balanced Split Flap

Flight Investigation of Internally Balanced Sealed Ailerons in the Presence of a Balanced Split Flap

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2.05, 2.54, and 2.04

Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2.05, 2.54, and 2.04

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
NACA Impact Basin and Water Landing Tests of a Float Model at Various Velocities and Weights

NACA Impact Basin and Water Landing Tests of a Float Model at Various Velocities and Weights

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effect of Initial Displacement of the Center Support on the Buckling of a Column Continuous Over Three Supports

Effect of Initial Displacement of the Center Support on the Buckling of a Column Continuous Over Three Supports

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Tensile Tests of NACA and Conventional Machine-countersunk Flush Rivets

Tensile Tests of NACA and Conventional Machine-countersunk Flush Rivets

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effects of Compressibility and Large Angles of Yaw on Pressure Indicated by a Total-pressure Tube

Effects of Compressibility and Large Angles of Yaw on Pressure Indicated by a Total-pressure Tube

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-foot-span Fighter-type Wing of NACA 230-series A

Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-foot-span Fighter-type Wing of NACA 230-series A

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Simple Method for Estimating Terminal Velocity Including Effect of Compressibility on Drag

Simple Method for Estimating Terminal Velocity Including Effect of Compressibility on Drag

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Flight Tests of the Lateral Control Characteristics of an F6F-3 Airplane Equipped With Spring-tab Ailerons

Flight Tests of the Lateral Control Characteristics of an F6F-3 Airplane Equipped With Spring-tab Ailerons

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag

Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Airfoil-contour Modifications Based on [epsilon]-curve Method of Calculating Pressure Distribution

Airfoil-contour Modifications Based on [epsilon]-curve Method of Calculating Pressure Distribution

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
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 A

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 A

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
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

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered With Camouflage Paint

Flight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered With Camouflage Paint

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Flight Studies of the Horizontal-tail Loads Experienced by a Modern Pursuit Airplane in Abrupt Maneuvers

Flight Studies of the Horizontal-tail Loads Experienced by a Modern Pursuit Airplane in Abrupt Maneuvers

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012 Airfoil With Various Type

Comparison of Pitching Moments Produced by Plain Flaps and by Spoilers and Some Aerodynamic Characteristics of an NACA 23012 Airfoil With Various Type

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Analysis of Available Data on the Effectiveness of Ailerons Without Exposed Overhang Balance

Analysis of Available Data on the Effectiveness of Ailerons Without Exposed Overhang Balance

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Wind-tunnel Investigation of Effects of a Pusher Propeller on Lift, Profile Drag, Pressure Distribution, and Boundary-layer Transition of a Flapped Wi

Wind-tunnel Investigation of Effects of a Pusher Propeller on Lift, Profile Drag, Pressure Distribution, and Boundary-layer Transition of a Flapped Wi

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Stability in a Body Stabilized by Fins and Suspended From an Airplane

Stability in a Body Stabilized by Fins and Suspended From an Airplane

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Method for Studying the Hunting Oscillations of an Airplane With a Simple Type of Automatic Control

Method for Studying the Hunting Oscillations of an Airplane With a Simple Type of Automatic Control

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Theoretical Determination of Low-drag Supercavitating Hydrofoils and Their Two-dimensional Characteristics at Zero Cavitation Number

Theoretical Determination of Low-drag Supercavitating Hydrofoils and Their Two-dimensional Characteristics at Zero Cavitation Number

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel

Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effect of the Lift Coefficient on Propeller Flutter

Effect of the Lift Coefficient on Propeller Flutter

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Flight Measurements of the Rudder Control and Sideslip Characteristics of Four Vertical Tail Arrangements on the P-40 Series Airplanes

Flight Measurements of the Rudder Control and Sideslip Characteristics of Four Vertical Tail Arrangements on the P-40 Series Airplanes

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effect of Lateral Area on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Langley Free-fligh

Effect of Lateral Area on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Langley Free-fligh

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effect of Compressibility on the Hovering Performance of Two 10-foot-diameter Helicopter Rotors Tested in the Langley Full-scale Tunnel

Effect of Compressibility on the Hovering Performance of Two 10-foot-diameter Helicopter Rotors Tested in the Langley Full-scale Tunnel

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Emergency Measures for Increasing the Range of Fighter Airplanes

Emergency Measures for Increasing the Range of Fighter Airplanes

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Experiments on Drag of Revolving Disks, Cylinders and Streamline Rods at High Speeds

Experiments on Drag of Revolving Disks, Cylinders and Streamline Rods at High Speeds

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Charts for the Determination of Wing Torsional Stiffness Required for Specified Rolling Characteristics or Aileron Reversal Speed

Charts for the Determination of Wing Torsional Stiffness Required for Specified Rolling Characteristics or Aileron Reversal Speed

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Electromagnetic-analogy Method of Solving Lifting-surface-theory Problems

Electromagnetic-analogy Method of Solving Lifting-surface-theory Problems

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels With Z-section Stiffeners.: I, Panels With Close Stiffener Spaci

Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels With Z-section Stiffeners.: I, Panels With Close Stiffener Spaci

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Approximate Determination of the Power Required to Move Control Surfaces as Related to Control-booster Design

Approximate Determination of the Power Required to Move Control Surfaces as Related to Control-booster Design

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Effect of Compressibility on the Pressures and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0.20-chord Flap

Effect of Compressibility on the Pressures and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0.20-chord Flap

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
On Slender-body Theory at Transonic Speeds

On Slender-body Theory at Transonic Speeds

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 25,06
Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane

Wind-tunnel Investigation of the Aerodynamic and Structural Deflection Characteristics of the Goodyear Inflatoplane

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Langley Full-scale-tunnel Tests of the Custer Channel Wing Airplane

Langley Full-scale-tunnel Tests of the Custer Channel Wing Airplane

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Wind-tunnel Tests of a Blunt-nose Aileron With Beveled Trailing Edge on an NACA 66(215)-216 Airfoil With Several Modifications of Aileron Nose and Adj

Wind-tunnel Tests of a Blunt-nose Aileron With Beveled Trailing Edge on an NACA 66(215)-216 Airfoil With Several Modifications of Aileron Nose and Adj

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Data for Design of Entrance Vanes From Two-dimensional Tests of Airfoils in Cascade

Data for Design of Entrance Vanes From Two-dimensional Tests of Airfoils in Cascade

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Determination of the Effect of Horizontal-tail Flexibility on Longitudinal Control Characteristics

Determination of the Effect of Horizontal-tail Flexibility on Longitudinal Control Characteristics

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Theory of Propellers.: I, Determination of the Circulation Function and the Mass Coefficient for Dual-rotating Propellers

Theory of Propellers.: I, Determination of the Circulation Function and the Mass Coefficient for Dual-rotating Propellers

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Tables and Charts for the Evaluation of Profile Drag From Wake Surveys at High Subsonic Speeds

Tables and Charts for the Evaluation of Profile Drag From Wake Surveys at High Subsonic Speeds

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Climb and High-speed Tests of a Curtiss No. 714-1C2-12 Four-blade Propeller on the Republic P-47C Airplane

Climb and High-speed Tests of a Curtiss No. 714-1C2-12 Four-blade Propeller on the Republic P-47C Airplane

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Frequency of Occurrence of Atmospheric Gusts and of Related Loads on Airplane Structures

Frequency of Occurrence of Atmospheric Gusts and of Related Loads on Airplane Structures

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Flight Investigation of NACA Aileron Modifications for the Improvement of the Lateral Control Characterisitcs of a High-speed Fighter Airplance

Flight Investigation of NACA Aileron Modifications for the Improvement of the Lateral Control Characterisitcs of a High-speed Fighter Airplance

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Theory of Propellers.: III, the Slipstream Contraction With Numerical Values for Two-blade and Four-blade Propellers

Theory of Propellers.: III, the Slipstream Contraction With Numerical Values for Two-blade and Four-blade Propellers

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 29,50
Effects of Heat-capacity Lag in Gas Dynamics

Effects of Heat-capacity Lag in Gas Dynamics

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 27,28
Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating Near the Free Water Surface

Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating Near the Free Water Surface

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 29,50
Conformal Transformation of an Airfoil Into a Straight Line and Its Application to the Inverse Problem of Airfoil Theory

Conformal Transformation of an Airfoil Into a Straight Line and Its Application to the Inverse Problem of Airfoil Theory

Langley Aeronautical Laboratory
Hassell Street Press, Paperback, New

€ 29,50
Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel

Aerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils From Tests in the NACA Two-dimensional Low-turbulence Pressure Tunnel

Langley Aeronautical Laboratory
Hassell Street Press, Hardcover, New

€ 39,51
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