Tank Tests To Determine The Effect Of Varying Design Parameters Of Planing Tail Hulls

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Tank Tests To Determine The Effect Of Varying Design Parameters Of Planing Tail Hulls
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Author : John R. Dawson
language : en
Publisher:
Release Date : 1946
Tank Tests To Determine The Effect Of Varying Design Parameters Of Planing Tail Hulls written by John R. Dawson and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Seaplanes categories.
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.
Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1949
Index Of Naca Technical Publications written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1949 with Aeronautics categories.
Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1952
Technical Note National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Aeronautics categories.
Naca Industry Conference On Personal Aircraft Research
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1946
Naca Industry Conference On Personal Aircraft Research written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Aeronautics categories.
Aerodynamic Characteristics Of Three Planing Tail Flying Boat Hulls
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Author : Campbell C. Yates
language : en
Publisher:
Release Date : 1947
Aerodynamic Characteristics Of Three Planing Tail Flying Boat Hulls written by Campbell C. Yates and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1947 with Airplanes categories.
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.
Investigation Of The Air Compression Process During Drop Tests Of An Oleo Pneumatic Landing Gear
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Author : James H. Walls
language : en
Publisher:
Release Date : 1951
Investigation Of The Air Compression Process During Drop Tests Of An Oleo Pneumatic Landing Gear written by James H. Walls and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1951 with Airplanes categories.
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.
Technical Note
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Author :
language : en
Publisher:
Release Date : 1948
Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1948 with Aeronautics categories.
Report National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1946
Report National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Aeronautics categories.
Annual Report Of The National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1950
Annual Report Of The National Advisory Committee For Aeronautics written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1950 with Aeronautics categories.
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Report
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1946
Report written by United States. National Advisory Committee for Aeronautics and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1946 with Aeronautics categories.