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Langley Aeronautical Laboratory

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Aerodynamics--Research.Investigation of effect of sideslip on lateral stability characteristics.Langley Aeronautical Laboratory

Investigation of effect of sideslip on lateral stability characteristics.

Langley Aeronautical Laboratory · Langley Memorial Aeronautical Laboratory

62 sayfa · 1944

Airplanes--Fuselage--Testing / Airplanes--Wings--Testing / Aerodynamics--Research.

Aerodynamics--Research.Theory of propellers.Langley Aeronautical Laboratory

Theory of propellers.

Langley Aeronautical Laboratory · Langley Memorial Aeronautical Laboratory

112 sayfa · 1944

Propellers, Aerial / Aerodynamics--Research.

CiltWind-Tunnel Investigation of Control-surface CharacteristicsLangley Aeronautical Laboratory

Wind-Tunnel Investigation of Control-surface Characteristics

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltTheory of PropellersLangley Aeronautical Laboratory

Theory of Propellers

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2023

Kategori yok

CiltTheory of PropellersLangley Aeronautical Laboratory

Theory of Propellers

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltAerodynamic Characteristics of the NACA 747A315 and 747A415 Airfoils from Tests in the NACA Two-Dimensional Low-turbulence Pressure TunnelLangley Aeronautical Laboratory

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

Langley Aeronautical Laboratory · Langley Memorial Aeronautical Laboratory

24 sayfa · 1944

Kategori yok

Aerodynamics--Research.Hinge moments of sealed-internal-balance arrangements for control surfaces.Langley Aeronautical Laboratory

Hinge moments of sealed-internal-balance arrangements for control surfaces.

Langley Aeronautical Laboratory · Langley Memorial Aeronautical Laboratory

54 sayfa · 1945

Airplanes--Wings--Testing / Aerodynamics--Research.

Flutter (Aerodynamics)Aerodynamic theory and its application to flutterLangley Aeronautical Laboratory.

Aerodynamic theory and its application to flutter

Langley Aeronautical Laboratory. · National Advisory Committee for Aeronautics

26 sayfa · 1956

Flutter (Aerodynamics)

CiltSummary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-Speed MissilesLangley Aeronautical Laboratory

Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-Speed Missiles

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltFlight Investigation of NACA Aileron Modifications for the Improvement of the Lateral Control Characterisitcs of a High-Speed Fighter AirplanceLangley Aeronautical Laboratory

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

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltDetermination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-flight TunnelLangley Aeronautical Laboratory

Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-flight Tunnel

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltEffect of the Lift Coefficient on Propeller FlutterLangley Aeronautical Laboratory

Effect of the Lift Coefficient on Propeller Flutter

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltFlight Investigation at High Speeds of Profile Drag of Wing of a P-47D Airplane Having Production Surfaces Covered with Camouflage PaintLangley Aeronautical Laboratory

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 · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltSupersonic-Tunnel Tests of Projectiles in Germany and ItalyLangley Aeronautical Laboratory

Supersonic-Tunnel Tests of Projectiles in Germany and Italy

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltPressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2. 05, 2. 54, And 2. 04Langley Aeronautical Laboratory

Pressure Distribution and Pressure Drag for a Hemispherical Nose at Mach Numbers 2. 05, 2. 54, And 2. 04

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltHeat Transfer and Pressure Measurement on a 5-Inch Hemispherical Concave Nose at a Mach Number Of 2. 0Langley Aeronautical Laboratory

Heat Transfer and Pressure Measurement on a 5-Inch Hemispherical Concave Nose at a Mach Number Of 2. 0

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

Kategori yok

CiltGeneral Solutions of Optimum Problems in Nonstationary FlightLangley Aeronautical Laboratory

General Solutions of Optimum Problems in Nonstationary Flight

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltCorrelation of Supersonic Convective Heat-Transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)Langley Aeronautical Laboratory

Correlation of Supersonic Convective Heat-Transfer Coefficients from Measurements of the Skin Temperature of a Parabolic Body of Revolution (NACA RM-10)

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltHinge Moments of Sealed-Internal-balance Arrangements for Control SurfacesLangley Aeronautical Laboratory

Hinge Moments of Sealed-Internal-balance Arrangements for Control Surfaces

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltExperimental Determination of the Effect of Negative Dihedral on Lateral Stability and Control Characteristics at High Lift CoefficientsLangley Aeronautical Laboratory

Experimental Determination of the Effect of Negative Dihedral on Lateral Stability and Control Characteristics at High Lift Coefficients

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

Kategori yok

CiltFlight Studies of the Horizontal-Tail Loads Experienced by a Modern Pursuit Airplane in Abrupt ManeuversLangley Aeronautical Laboratory

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

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltFormulas for Propellers in Yaw and Charts on the Side-Force DerivativeLangley Aeronautical Laboratory

Formulas for Propellers in Yaw and Charts on the Side-Force Derivative

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

Kategori yok

CiltWind-Tunnel Tests of a Dual-rotating Propeller Having One Component Locked or WindmillingLangley Aeronautical Laboratory

Wind-Tunnel Tests of a Dual-rotating Propeller Having One Component Locked or Windmilling

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

Kategori yok

CiltTheoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating near the Free Water SurfaceLangley Aeronautical Laboratory

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

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2023

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CiltInvestigation of Methods of Supporting Single-Thickness Specimens in a Fixture for Determination of Compressive Stress-strain CurvesLangley Aeronautical Laboratory

Investigation of Methods of Supporting Single-Thickness Specimens in a Fixture for Determination of Compressive Stress-strain Curves

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltEffect of Compressibility on the Pressures and Forces Acting on a Modified NACA 65,3-019 Airfoil Having a 0. 20-Chord FlapLangley Aeronautical Laboratory

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 · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltWind-Tunnel Investigation of a Rectangular NACA 2212 Airfoil with Semispan Ailerons and with Nonperforated, Balanced Double Split Flaps for Use As Aerodynamic BrakesLangley Aeronautical Laboratory

Wind-Tunnel Investigation of a Rectangular NACA 2212 Airfoil with Semispan Ailerons and with Nonperforated, Balanced Double Split Flaps for Use As Aerodynamic Brakes

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltWind-Tunnel Investigation of an NACA 23021 Airfoil with a 0. 32-airfoil-chord Double Slotted FlapLangley Aeronautical Laboratory

Wind-Tunnel Investigation of an NACA 23021 Airfoil with a 0. 32-airfoil-chord Double Slotted Flap

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

Kategori yok

CiltFree-Flight Measurements of Aerodynamic Heat Transfer to Mach Number 3. 9 and of Drag to Mach Number 6. 9 of a Fin-stabilized Cone-cylinder ConfigurationLangley Aeronautical Laboratory

Free-Flight Measurements of Aerodynamic Heat Transfer to Mach Number 3. 9 and of Drag to Mach Number 6. 9 of a Fin-stabilized Cone-cylinder Configuration

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltLifting-Surface-theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick ForcesLangley Aeronautical Laboratory

Lifting-Surface-theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick Forces

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

Kategori yok