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Tank Tests To Determine The Effect Of Varying Design Parameters Of Planing Tail Hulls
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Book Synopsis Tank Tests to Determine the Effect of Varying Design Parameters of Planing-tail Hulls by : John R. Dawson
Download or read book Tank Tests to Determine the Effect of Varying Design Parameters of Planing-tail Hulls written by John R. Dawson and published by . This book was released on 1946 with total page 582 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second part of a series of tests made in Langley tank no. 2 to determine the effect of varying design parameters of planing-tail hulls is presented. Results are given to show the effects on resistance characteristics of varying angle of afterbody keel, depth of step, and length of afterbody chine. The effect of varying the gross load is shown for one configuration. The resistance characteristics of planing-tail hulls are compared withthose of a conventional flying-boat hull. The forces on the forebody and afterbody of one configuration are compared with the forces on a conventional hull.
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Impact Strength and Flexural Properties of Laminated Plastics at High and Low Temperatures by : J. J. Lamb
Download or read book Impact Strength and Flexural Properties of Laminated Plastics at High and Low Temperatures written by J. J. Lamb and published by . This book was released on 1946 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Izod-impact strengths and flexural properties of several types of plastic laminates, which are either in use or have potential application in aircraft structures and parts, were determined at different temperatures in the range of -70 degrees to 200 degrees F.
Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 898 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Three Planing-tail Flying-boat Hulls by : Campbell C. Yates
Download or read book Aerodynamic Characteristics of Three Planing-tail Flying-boat Hulls written by Campbell C. Yates and published by . This book was released on 1947 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made to determine the aerodynamic characteristics of three planing-tail flying-boat hulls which differed only in the amount of step fairing. The hulls were derived by altering the step and afterbody of a conventional flying-boat hull having a transverse step.
Book Synopsis NACA-Industry Conference on Personal-Aircraft Research by : United States. National Advisory Committee for Aeronautics
Download or read book NACA-Industry Conference on Personal-Aircraft Research written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Air-compression Process During Drop Tests of an Oleo-pneumatic Landing Gear by : James H. Walls
Download or read book Investigation of the Air-compression Process During Drop Tests of an Oleo-pneumatic Landing Gear written by James H. Walls and published by . This book was released on 1951 with total page 788 pages. Available in PDF, EPUB and Kindle. Book excerpt: A brief study has been made to evaluate the importance of the type of air-compression process on the loads produced on an oleo-pneumatic landing gear during impact and to determine the type of air compression process actually obtained during drop tests. A simplified analysis to determine the effect which different air-compression processes might have indicates that the value of the air-compression exponent should have relatively little effect on the landing-gear loads throughout most of the impact. The analysis of experimental data obtained in these tests shows that the polytropic exponent ranged from 1.01 to 1.10 for the condtions tested. The general trend of the data appears relatively independent of vertical contact velocity.
Download or read book Technical Note written by and published by . This book was released on 1946 with total page 460 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Annual Report of the National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics
Download or read book Annual Report of the National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1945 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Book Synopsis Report by : United States. National Advisory Committee for Aeronautics
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Critical Combinations of Shear and Transverse Direct Stress for an Infinitely Long Flat Plate with Edges Elastically Restrained Against Rotation by : Antonio Ferri
Download or read book Critical Combinations of Shear and Transverse Direct Stress for an Infinitely Long Flat Plate with Edges Elastically Restrained Against Rotation written by Antonio Ferri and published by . This book was released on 1946 with total page 232 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Index of NACA Reports Having Application to Personal Aircraft by : United States. National Advisory Committee for Aeronautics
Download or read book Index of NACA Reports Having Application to Personal Aircraft written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1946 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Full-scale Investigation on the Blade Motion of the PV-2 Helicopter Rotor by : Eugene Migotsky
Download or read book Full-scale Investigation on the Blade Motion of the PV-2 Helicopter Rotor written by Eugene Migotsky and published by . This book was released on 1948 with total page 798 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the PV-2 helicopter rotor has been conducted at the Langley Laboratory of the National Advisory Committee for Aeronautics to determine the basic characteristics of a fully articulated rotor.
Book Synopsis The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight by : Richard Scherrer
Download or read book The Effects of Aerodynamic Heating and Heat Transfer on the Surface Temperature of a Body of Revolution in Steady Supersonic Flight written by Richard Scherrer and published by . This book was released on 1947 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt: An approximate method for determining the convective cooling requirement in the laminar-boundary-layer region of a body of revolution in high-speed flight was developed and applied to an example body. The cooling requirement for the example body was determined as a function of Mach number, altitude, size, and a surface-temperature parameter. The maximum value of Mach number considered was 3.0 and the altitudes considered were those within the lower constant-temperature region of the atmosphere (40,000 to 120,000 ft). The extent of the laminar boundary layer was determined approximately at each condition as a function of the variables considered.
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis List of Technical Notes, 1947-1953 by : United States. National Advisory Committee for Aeronautics
Download or read book List of Technical Notes, 1947-1953 written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:
