17,005 Documents in our Technical Library
2727426 Total Downloads

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...

naca-report-1075

naca-report-1075
  • Version
  • 167 Downloads
  • 897.60 KB File Size
  • 1 File Count
  • September 7, 2016 Create Date
  • September 7, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Hydrodynamic of a System with a Single Elastic Mode, II - Comparison of Experimental Force and Response with Theory

naca-report-1075 Hydrodynamic of a System with a Single Elastic Mode, II - Comparison of Experimental Force and Response with Theory-1

Hydrodynamic impact tests were made on an elastic model
approximating a t-wo-mass—spring system to determine experi—
mentally the efieets of structural flexibility on the hydrodynamic
loads encountered during seaplane landing impacts and to
correlate the results with theory. A flexible seaplane was
represented by a t-wo-mass—spring system consisting of a rigid
prismatic float connected to a rigid upper mass by an elastic
structure. The model had a ratio of sprung mass to hull mass
of 0.6 and a natural frequency of 3.0 cycles per second. The
tests were conducted in smooth water at fixed. trims and included
both high and low flight-path angles and a range of relocity.

The results of the tests are compared with theoretical time
histories of hydrodynamic impact force and elastic-system
response calculated by the method of NACA Rep. 1074 which
considers the applied hydrodynamic load and structural response
to be interdependent or coupled throughout the impact. The
hydrodynamic-fine time histories obtained with the elastic
system are also compared with the hydrodynamic-force time
histories that would have been obtained for the same initial
conditions if the system were rigid.

Experience with large airplanes has shown that the elastic
behavior of the structure during landing impact. may be a
critical design consideration. Analytical methods for treat-
ing landing impact of elastic structures have been developed,
but most of these methods assume that the external load
applied to the structure during impact is not influenced by
the elasticity of the structure and that the structural re-
sponse can be determined from the load that would have been
applied if the str'ucture were rigid. In reference 1, however,
an analytical method for treating hydrodynamic impact of
an elastic structure is presented in which interaction of the
applied load and structural response is included, and it is
shown that structural flexibility may have appreciable effects
on the applied load.

FileAction
naca-report-1075 Hydrodynamic of a System with a Single Elastic Mode, II - Comparison of Experimental Force and Response with Theory.pdfDownload 

Comment On This Post

Your email address will not be published. Required fields are marked *

naca-report-1075

naca-report-1075
  • Version
  • 167 Downloads
  • 897.60 KB File Size
  • 1 File Count
  • September 7, 2016 Create Date
  • September 7, 2016 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Report - Hydrodynamic of a System with a Single Elastic Mode, II - Comparison of Experimental Force and Response with Theory

naca-report-1075 Hydrodynamic of a System with a Single Elastic Mode, II - Comparison of Experimental Force and Response with Theory-1

Hydrodynamic impact tests were made on an elastic model
approximating a t-wo-mass—spring system to determine experi—
mentally the efieets of structural flexibility on the hydrodynamic
loads encountered during seaplane landing impacts and to
correlate the results with theory. A flexible seaplane was
represented by a t-wo-mass—spring system consisting of a rigid
prismatic float connected to a rigid upper mass by an elastic
structure. The model had a ratio of sprung mass to hull mass
of 0.6 and a natural frequency of 3.0 cycles per second. The
tests were conducted in smooth water at fixed. trims and included
both high and low flight-path angles and a range of relocity.

The results of the tests are compared with theoretical time
histories of hydrodynamic impact force and elastic-system
response calculated by the method of NACA Rep. 1074 which
considers the applied hydrodynamic load and structural response
to be interdependent or coupled throughout the impact. The
hydrodynamic-fine time histories obtained with the elastic
system are also compared with the hydrodynamic-force time
histories that would have been obtained for the same initial
conditions if the system were rigid.

Experience with large airplanes has shown that the elastic
behavior of the structure during landing impact. may be a
critical design consideration. Analytical methods for treat-
ing landing impact of elastic structures have been developed,
but most of these methods assume that the external load
applied to the structure during impact is not influenced by
the elasticity of the structure and that the structural re-
sponse can be determined from the load that would have been
applied if the str'ucture were rigid. In reference 1, however,
an analytical method for treating hydrodynamic impact of
an elastic structure is presented in which interaction of the
applied load and structural response is included, and it is
shown that structural flexibility may have appreciable effects
on the applied load.

FileAction
naca-report-1075 Hydrodynamic of a System with a Single Elastic Mode, II - Comparison of Experimental Force and Response with Theory.pdfDownload 
17,005 Documents in our Technical Library
2727426 Total Downloads

Search The Technical Library

Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...