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Langley Aeronautical Laboratory

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Effect of Normal Pressure on the Critical Shear Stress of Curved Sheet

Langley Aeronautical Laboratory · Hassell Street Press

26 sayfa · 2021

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Study of the Flow Over a 45° Sweptback Wing -fuselage Combination at Transonic Mach Numbers

Langley Aeronautical Laboratory · Hassell Street Press

68 sayfa · 2021

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Considerations of Wake-excited Vibratory Stress in a Pusher Propeller

Langley Aeronautical Laboratory · Hassell Street Press

32 sayfa · 2021

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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

Langley Aeronautical Laboratory · Hassell Street Press

26 sayfa · 2021

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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

Langley Aeronautical Laboratory · Hassell Street Press

38 sayfa · 2021

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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

Langley Aeronautical Laboratory · Hassell Street Press

32 sayfa · 2021

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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.

CiltTheory of PropellersLangley Aeronautical Laboratory

Theory of Propellers

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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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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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 · Creative Media Partners, LLC

24 sayfa · 1944

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CiltTheory of PropellersLangley Aeronautical Laboratory

Theory of Propellers

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2023

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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.

WingsRecent research on the determination of natural modes and frequencies of aircraft wing structuresLangley Aeronautical Laboratory.

Recent research on the determination of natural modes and frequencies of aircraft wing structures

Langley Aeronautical Laboratory. · National Advisory Committee for Aeronautics

21 sayfa · 1956

Airplanes / Vibration (Aeronautics) / Wings

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)

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 · 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

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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

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CiltEffect of Hinge-Moment Parameters on Elevator Stick Forces in Rapid ManeuversLangley Aeronautical Laboratory

Effect of Hinge-Moment Parameters on Elevator Stick Forces in Rapid Maneuvers

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltSome Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave DragLangley Aeronautical Laboratory

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

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltInfluence of Vertical-Tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin-engine-airplane Model with One Engine InoperativeLangley Aeronautical Laboratory

Influence of Vertical-Tail Design and Direction of Propeller Rotation on Trim Characteristics of a Twin-engine-airplane Model with One Engine Inoperative

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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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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CiltEffects of Roughness at High Reynolds Numbers on the Lift and Drag Characteristics of Three Thick AirfoilsLangley Aeronautical Laboratory

Effects of Roughness at High Reynolds Numbers on the Lift and Drag Characteristics of Three Thick Airfoils

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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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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CiltEffects of Specific Types of Surface Roughness on Boundary-Layer TransitionLangley Aeronautical Laboratory

Effects of Specific Types of Surface Roughness on Boundary-Layer Transition

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltFlight Investigation of Boundary-Layer Transition and Profile Drag of an Experimental Low-drag Wing Installed on a Fighter-type AirplaneLangley Aeronautical Laboratory

Flight Investigation of Boundary-Layer Transition and Profile Drag of an Experimental Low-drag Wing Installed on a Fighter-type Airplane

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltEffect of High Wing Loading on Landing Technique and Distance, with Experimental Data for the B-26 AirplaneLangley Aeronautical Laboratory

Effect of High Wing Loading on Landing Technique and Distance, with Experimental Data for the B-26 Airplane

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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CiltEffect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels with Z-Section StiffenersLangley Aeronautical Laboratory

Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels with Z-Section Stiffeners

Langley Aeronautical Laboratory · Creative Media Partners, LLC

Sayfa sayısı yok · 2021

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