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Showing 1 - 25 of 123 matches in All Departments

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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Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-speed... Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-speed Missiles (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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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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Wind-tunnel Investigation of Control-surface Characteristics. - XVI, Pressure Distribution Over an NACA 0009 Airfoil With... Wind-tunnel Investigation of Control-surface Characteristics. - XVI, Pressure Distribution Over an NACA 0009 Airfoil With 0.30-airfoil-chord Beveled-trailing-edge Flaps (Paperback)
Langley Aeronautical Laboratory
R462 Discovery Miles 4 620
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Influence of Vertical-tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin-engine-airplane Model... Influence of Vertical-tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin-engine-airplane Model With One Engine Inoperative (Paperback)
Langley Aeronautical Laboratory
R403 Discovery Miles 4 030
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Effect of High Wing Loading on Landing Technique and Distance, With Experimental Data for the B-26 Airplane (Paperback):... Effect of High Wing Loading on Landing Technique and Distance, With Experimental Data for the B-26 Airplane (Paperback)
Langley Aeronautical Laboratory
R456 Discovery Miles 4 560
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Application of Spring Tabs to Elevator Controls (Paperback): Langley Aeronautical Laboratory Application of Spring Tabs to Elevator Controls (Paperback)
Langley Aeronautical Laboratory
R343 Discovery Miles 3 430
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Emergency Measures for Increasing the Range of Fighter Airplanes (Paperback): Langley Aeronautical Laboratory Emergency Measures for Increasing the Range of Fighter Airplanes (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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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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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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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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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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Effect of Initial Displacement of the Center Support on the Buckling of a Column Continuous Over Three Supports (Paperback):... Effect of Initial Displacement of the Center Support on the Buckling of a Column Continuous Over Three Supports (Paperback)
Langley Aeronautical Laboratory
R340 Discovery Miles 3 400
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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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Profile-drag Coefficients of Conventional and Low-drag Airfoils as Obtained in Flight (Paperback): Langley Aeronautical... Profile-drag Coefficients of Conventional and Low-drag Airfoils as Obtained in Flight (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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Flight Investigation of Internally Balanced Sealed Ailerons in the Presence of a Balanced Split Flap (Paperback): Langley... Flight Investigation of Internally Balanced Sealed Ailerons in the Presence of a Balanced Split Flap (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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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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Some Notes on the Determination of the Stick-free Neutral Point From Wind-tunnel Data (Paperback): Langley Aeronautical... Some Notes on the Determination of the Stick-free Neutral Point From Wind-tunnel Data (Paperback)
Langley Aeronautical Laboratory
R339 Discovery Miles 3 390
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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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Numerical Evaluation of the Wake-survey Equations for Subsonic Flow Including the Effect of Energy Addition (Paperback):... Numerical Evaluation of the Wake-survey Equations for Subsonic Flow Including the Effect of Energy Addition (Paperback)
Langley Aeronautical Laboratory
R406 Discovery Miles 4 060
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Prediction of Motions of an Airplane Resulting From Abrupt Movement of Lateral or Directional Controls (Paperback): Langley... Prediction of Motions of an Airplane Resulting From Abrupt Movement of Lateral or Directional Controls (Paperback)
Langley Aeronautical Laboratory
R342 Discovery Miles 3 420
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