Hydrodynamic Properties Of Planing Surfaces And Flying Boats

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Hydrodynamic Properties of Planing Surfaces and Flying Boats

Nikolaĭ Aleksandrovich Sokolov
Hydrodynamic Properties of Planing Surfaces and Flying Boats Book PDF

Author : Nikolaĭ Aleksandrovich Sokolov
Publisher : Unknown
Page : 64 pages
File Size : 41,9 Mb
Release : 1950
Category : Hydrodynamics
ISBN : UVA:X006080246

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Hydrodynamic Properties of Planing Surfaces and Flying Boats by Nikolaĭ Aleksandrovich Sokolov Pdf

The study of the hydrodynamic properties of planing bottom of flying boats and seaplane floats is at the present time based exclusively on the curves of towing tests conducted in tanks.

Report

Anonim
Report Book PDF

Author : Anonim
Publisher : Unknown
Page : 1180 pages
File Size : 51,6 Mb
Release : 1957
Category : Aeronautics
ISBN : MINN:31951D00028212O

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Report by Anonim Pdf

Report

United States. National Advisory Committee for Aeronautics
Report Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 56 pages
File Size : 55,7 Mb
Release : 1958
Category : Aeronautics
ISBN : STANFORD:36105024792934

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Report by United States. National Advisory Committee for Aeronautics Pdf

Annual Report - National Advisory Committee for Aeronautics

United States. National Advisory Committee for Aeronautics
Annual Report National Advisory Committee for Aeronautics Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 128 pages
File Size : 42,9 Mb
Release : 1957
Category : Aeronautics
ISBN : STANFORD:36105024166147

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Annual Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

An Experimental Investigation of Sting-support Effects on Drag and a Comparison with Jet Effects at Transonic Speeds

Charles L. Shuford,Edmund R. Jonash,Jack B. Esgar,Maurice S. Cahn,Robert F. Coleman,United States. National Advisory Committee for Aeronautics,Arnold M. Feingold,Eugene F. Schum,Jerrold D. Wear,Arthur N. Curren,William P. Cook
An Experimental Investigation of Sting support Effects on Drag and a Comparison with Jet Effects at Transonic Speeds Book PDF

Author : Charles L. Shuford,Edmund R. Jonash,Jack B. Esgar,Maurice S. Cahn,Robert F. Coleman,United States. National Advisory Committee for Aeronautics,Arnold M. Feingold,Eugene F. Schum,Jerrold D. Wear,Arthur N. Curren,William P. Cook
Publisher : Unknown
Page : 178 pages
File Size : 54,8 Mb
Release : 1958
Category : Aeronautics
ISBN : OSU:32435063879019

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An Experimental Investigation of Sting-support Effects on Drag and a Comparison with Jet Effects at Transonic Speeds by Charles L. Shuford,Edmund R. Jonash,Jack B. Esgar,Maurice S. Cahn,Robert F. Coleman,United States. National Advisory Committee for Aeronautics,Arnold M. Feingold,Eugene F. Schum,Jerrold D. Wear,Arthur N. Curren,William P. Cook Pdf

Technical Memorandums

United States. National Advisory Committee for Aeronautics
Technical Memorandums Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 458 pages
File Size : 46,8 Mb
Release : 1940
Category : Aeronautics
ISBN : UOM:39015020070481

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Technical Memorandums by United States. National Advisory Committee for Aeronautics Pdf

Chiefly translations from foreign aeronautical journals.

Two-dimensional Wing Theory in the Supersonic Range

H. Hönl
Two dimensional Wing Theory in the Supersonic Range Book PDF

Author : H. Hönl
Publisher : Unknown
Page : 764 pages
File Size : 41,7 Mb
Release : 1949
Category : Aerodynamic load
ISBN : STANFORD:36105024833944

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Two-dimensional Wing Theory in the Supersonic Range by H. Hönl Pdf

The plane problem of the vibrating airfoil in supersonic flow is dealt with and solved within the scope of a linearized theory by the method of the acceleration potential.

Technical Memorandum - National Advisory Committee for Aeronautics

United States. National Advisory Committee for Aeronautics
Technical Memorandum National Advisory Committee for Aeronautics Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 446 pages
File Size : 51,8 Mb
Release : 1940
Category : Aeronautics
ISBN : UIUC:30112018292901

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Technical Memorandum - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Chiefly translations from foreign aeronautical journals.

Aerodynamic Loads on a Leading-edge Flap and a Leading-edge Slat on the NACA 64A010 Airfoil Section

John A. Kelly,George B. McCullough
Aerodynamic Loads on a Leading edge Flap and a Leading edge Slat on the NACA 64A010 Airfoil Section Book PDF

Author : John A. Kelly,George B. McCullough
Publisher : Unknown
Page : 706 pages
File Size : 53,6 Mb
Release : 1954
Category : Aerodynamic load
ISBN : STANFORD:36105024831849

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Aerodynamic Loads on a Leading-edge Flap and a Leading-edge Slat on the NACA 64A010 Airfoil Section by John A. Kelly,George B. McCullough Pdf

A previous report, NACA TN 3007, gave force and moment data for the NACA 64A010 airfoil section equipped alternately with a flap and a slat at the leading edge, and with a split flap and a double-slotted flap at the trailing edge. The present report presents the chordwise distributions of pressure measured concurrently with the force and moment data of NACA 3007. The pressure data for the leading-edge flap and slat have been converted into coefficients of normal force, chord force, and moment based on the geometry of the leading-edge device.

Technical Note - National Advisory Committee for Aeronautics

United States. National Advisory Committee for Aeronautics
Technical Note National Advisory Committee for Aeronautics Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 530 pages
File Size : 43,6 Mb
Release : 1957
Category : Aeronautics
ISBN : OSU:32435026187765

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Technical Note - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Experimental Study of Heat Transfer to Small Cylinders in a Subsonic, High-temperature Gas Stream

George E. Glawe,Robert C. Johnson
Experimental Study of Heat Transfer to Small Cylinders in a Subsonic High temperature Gas Stream Book PDF

Author : George E. Glawe,Robert C. Johnson
Publisher : Unknown
Page : 820 pages
File Size : 53,8 Mb
Release : 1957
Category : Combustion gases
ISBN : STANFORD:36105024832276

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Experimental Study of Heat Transfer to Small Cylinders in a Subsonic, High-temperature Gas Stream by George E. Glawe,Robert C. Johnson Pdf

A Nusselt-Reynolds number relation for cylindrical thermocouple wires in crossflow was obtained from the experimental determination of time constants. Tests were conducted in exhaust gas over a temperature range of 2000 to 3400 R, a Mach number range of 0.3 to 0.8, and a static-pressure range from 2/3 to 1-1/3 atmospheres, yielding a Reynolds number range of 450 to 3000. The correlation obtained is Nu=(0.428 plus or minus 0.003) times the square root of Re with average deviations of a single observation of 8.5 percent. This relation is the same as one previously reported for room-temperature conditions.

FAA Thesaurus of Technical Descriptors

United States. Federal Aviation Administration
FAA Thesaurus of Technical Descriptors Book PDF

Author : United States. Federal Aviation Administration
Publisher : Unknown
Page : 72 pages
File Size : 54,9 Mb
Release : 1969
Category : Aeronautics, Commercial
ISBN : UCBK:C101351750

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FAA Thesaurus of Technical Descriptors by United States. Federal Aviation Administration Pdf