Langley Aeronautical Laboratory

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24 featured books

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OL9964631A

Overview

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24 representative editions

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Catalog identity

How this author appears inside the active Bookitis catalog.

Display name
Langley Aeronautical Laboratory
Source identifier
OL9964631A

Featured books

Representative editions for works actually authored by this person.

CO
Image source: Open Library
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
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 | 2021
Representative edition for this work grouping in the active catalog.
cover
EI
Image source: Open Library
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
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 | 2021
Representative edition for this work grouping in the active catalog.
cover
WI
Image source: Open Library
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
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 | 2021
Representative edition for this work grouping in the active catalog.
cover
EO
Image source: Open Library
Effect of Normal Pressure on the Critical Shear Stress of Curved Sheet
Effect of Normal Pressure on the Critical Shear Stress of Curved Sheet | 2021
Representative edition for this work grouping in the active catalog.
cover
SO
Image source: Open Library
Study of the Flow Over a 45° Sweptback Wing -fuselage Combination at Transonic Mach Numbers
Study of the Flow Over a 45° Sweptback Wing -fuselage Combination at Transonic Mach Numbers | 2021
Representative edition for this work grouping in the active catalog.
cover
CO
Image source: Open Library
Considerations of Wake-excited Vibratory Stress in a Pusher Propeller
Considerations of Wake-excited Vibratory Stress in a Pusher Propeller | 2021
Representative edition for this work grouping in the active catalog.
cover
Theory of PropellersLangley Aeronautical Laboratory
TO
Theory of Propellers
Theory of Propellers | 2023
Representative edition for this work grouping in the active catalog.
no cover
Heat Transfer and Skin Friction...Langley Aeronautical Laboratory
HT
Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds
Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds | 2023
Representative edition for this work grouping in the active catalog.
no cover
Theoretical and Experimental In...Langley Aeronautical Laboratory
TA
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 | 2023
Representative edition for this work grouping in the active catalog.
no cover
Comparison of Wind-Tunnel and F...Langley Aeronautical Laboratory
CO
Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas a-26 Airplane
Comparison of Wind-Tunnel and Flight Measurements of Stability and Control Characteristics of a Douglas a-26 Airplane | 2021
Representative edition for this work grouping in the active catalog.
no cover
On Slender-Body Theory at Trans...Langley Aeronautical Laboratory
OS
On Slender-Body Theory at Transonic Speeds
On Slender-Body Theory at Transonic Speeds | 2021
Representative edition for this work grouping in the active catalog.
no cover
Wind-Tunnel Investigation of Ro...Langley Aeronautical Laboratory
WI
Wind-Tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface
Wind-Tunnel Investigation of Rounded Horns and of Guards on a Horizontal Tail Surface | 2021
Representative edition for this work grouping in the active catalog.
no cover
Summary of Available Knowledge...Langley Aeronautical Laboratory
SO
Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-Speed Missiles
Summary of Available Knowledge Concerning Skin Friction and Heat Transfer and Its Application to the Design of High-Speed Missiles | 2021
Representative edition for this work grouping in the active catalog.
no cover
Flight Investigation of NACA Ai...Langley Aeronautical Laboratory
FI
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 | 2021
Representative edition for this work grouping in the active catalog.
no cover
Stability in a Body Stabilized...Langley Aeronautical Laboratory
SI
Stability in a Body Stabilized by Fins and Suspended from an Airplane
Stability in a Body Stabilized by Fins and Suspended from an Airplane | 2021
Representative edition for this work grouping in the active catalog.
no cover
Determination of the Stability...Langley Aeronautical Laboratory
DO
Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-flight Tunnel
Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-flight Tunnel | 2021
Representative edition for this work grouping in the active catalog.
no cover
Effect of the Lift Coefficient...Langley Aeronautical Laboratory
EO
Effect of the Lift Coefficient on Propeller Flutter
Effect of the Lift Coefficient on Propeller Flutter | 2021
Representative edition for this work grouping in the active catalog.
no cover
Flight Investigation at High Sp...Langley Aeronautical Laboratory
FI
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 | 2021
Representative edition for this work grouping in the active catalog.
no cover
Pressure Distribution and Press...Langley Aeronautical Laboratory
PD
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 | 2021
Representative edition for this work grouping in the active catalog.
no cover
Supersonic-Tunnel Tests of Proj...Langley Aeronautical Laboratory
ST
Supersonic-Tunnel Tests of Projectiles in Germany and Italy
Supersonic-Tunnel Tests of Projectiles in Germany and Italy | 2021
Representative edition for this work grouping in the active catalog.
no cover
Application of Spring Tabs to E...Langley Aeronautical Laboratory
AO
Application of Spring Tabs to Elevator Controls
Application of Spring Tabs to Elevator Controls | 2021
Representative edition for this work grouping in the active catalog.
no cover
Method for Studying the Hunting...Langley Aeronautical Laboratory
MF
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 | 2021
Representative edition for this work grouping in the active catalog.
no cover
Wind-Tunnel Investigation of an...Langley Aeronautical Laboratory
WI
Wind-Tunnel Investigation of an NACA 23021 Airfoil with a 0. 32-airfoil-chord Double Slotted Flap
Wind-Tunnel Investigation of an NACA 23021 Airfoil with a 0. 32-airfoil-chord Double Slotted Flap | 2021
Representative edition for this work grouping in the active catalog.
no cover
Some Examples of the Applicatio...Langley Aeronautical Laboratory
SE
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 | 2021
Representative edition for this work grouping in the active catalog.
no cover

Works in catalog

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