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Langley Aeronautical Laboratory

Kirjat ja teokset yhdessä paikassa: 129 kirjaa, julkaisuja vuosilta 2021-2023, suosituimpien joukossa Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds. Vertaile teosten hintoja ja tarkista saatavuus suomalaisista kirjakaupoista.

129 kirjaa

Kirjojen julkaisuhaarukka 2021-2023.

Heat Transfer and Skin Friction for Turbulent Boundary Layers on Heated or Cooled Surfaces at High Speeds
This is a technical report by the Langley Aeronautical Laboratory detailing the heat transfer and skin friction for turbulent boundary layers on heated or cooled surfaces at high speeds. This book is of interest to aerospace engineers, physicists, and those working in the field of heat transfer and fluid mechanics.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it.This work is in the "public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating Near the Free Water Surface
Explore the cutting-edge research being conducted at the Langley Aeronautical Laboratory in the field of naval engineering. This groundbreaking study examines the potential of supercavitating hydrofoils to improve the speed and agility of underwater vessels.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it.This work is in the "public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Theory of Propellers.: III, the Slipstream Contraction With Numerical Values for Two-blade and Four-blade Propellers
Theory of Propellers III is a comprehensive guide to the design and operation of propellers. The book is written by the Langley Aeronautical Laboratory and is based on decades of research and experimentation. It provides a theoretical basis for the design of propellers and includes numerical values for two-blade and four-blade designs. This book is an important resource for anyone interested in aerodynamics or aviation.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it.This work is in the "public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Theory of Propellers.: I, Determination of the Circulation Function and the Mass Coefficient for Dual-rotating Propellers
Originally published in 1917, this classic text on the aerodynamics of propellers was a landmark in the field of aeronautical engineering. With detailed explanations and rigorous mathematical analysis, it remains an essential resource for anyone interested in the theory and design of aircraft propulsion systems.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it.This work is in the "public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
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
2021
nidottu
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface.We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Flight Investigation of Wing-gun Fairings on a Fighter Type Airplane

Flight Investigation of Wing-gun Fairings on a Fighter Type Airplane

Langley Aeronautical Laboratory

Hassell Street Press
2021
nidottu
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface.We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Wind-tunnel Investigation of Control-surface Characteristics.: XVI, Pressure Distribution Over an NACA 0009 Airfoil With 0.30-airfoil-chord Beveled-tr
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface.We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
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
2021
nidottu
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface.We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.
Wind-tunnel Investigation of an NACA 23021 Airfoil With a 0.32-airfoil-chord Double Slotted Flap
This work has been selected by scholars as being culturally important and is part of the knowledge base of civilization as we know it.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. To ensure a quality reading experience, this work has been proofread and republished using a format that seamlessly blends the original graphical elements with text in an easy-to-read typeface.We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.