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Analysis Of Multicell Delta Wings On Cal Tech Analog Computer


Analysis Of Multicell Delta Wings On Cal Tech Analog Computer
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Analysis Of Multicell Delta Wings On Cal Tech Analog Computer


Analysis Of Multicell Delta Wings On Cal Tech Analog Computer
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Author : Richard H. MacNeal
language : en
Publisher:
Release Date : 1953

Analysis Of Multicell Delta Wings On Cal Tech Analog Computer written by Richard H. MacNeal and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1953 with Airplanes categories.


Deflections and all internal forces have been calculated for concentrated static loads. Vibration modes are also presented. The effects of neglecting shearing strains in the ribs and spars and also of assuming the ribs to be rigid have been investigated by modifying the electric circuits to correspond to these simplifications.



Analysis Of Straight Multicell Wings On Cal Tech Analog Computer


Analysis Of Straight Multicell Wings On Cal Tech Analog Computer
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Author : Stanley U. Benscoter
language : en
Publisher:
Release Date : 1954

Analysis Of Straight Multicell Wings On Cal Tech Analog Computer written by Stanley U. Benscoter and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Electronic analog computers categories.


Using the Cal-Tech analog computer, structural analyses have been made for four straight multicell wings. Wings with aspect ratios of 2 and 4 and rectangular and biconvex cross sections have been considered. The wings are supported rigidly along two lines at the faces of the fuselage. Concentrated loads are applied at the interesection points of the ribs and spars. The effects of shearing strains in the ribs and spars are included. Deflections and all internal quantities have been recorded as well as vibration modes and frequencies.



Technical Note National Advisory Committee For Aeronautics


Technical Note National Advisory Committee For Aeronautics
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1957

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 1957 with Aeronautics categories.




Naca Research Memorandum


Naca Research Memorandum
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Author :
language : en
Publisher:
Release Date : 1955

Naca Research Memorandum written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Aerodynamics categories.




Experimental Analysis Of Multicell Wings By Means Of Plastic Models


Experimental Analysis Of Multicell Wings By Means Of Plastic Models
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Author : George W. Zender
language : en
Publisher:
Release Date : 1955

Experimental Analysis Of Multicell Wings By Means Of Plastic Models written by George W. Zender and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1955 with Airplanes categories.


The stresses and deflections of a plastic model of a delta multicell wing are presented and compared with theoretical results obtained by the use of the Cal-Tech analog computer. The comparison indicates that valuable information may be obtained for experimental structural analyses from tests of plastic models.



A Selected Listing Of Nasa Scientific And Technical Reports For


A Selected Listing Of Nasa Scientific And Technical Reports For
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Author :
language : en
Publisher:
Release Date : 1949

A Selected Listing Of Nasa Scientific And Technical Reports For written by 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.




Index Of Naca Technical Publications


Index Of Naca Technical Publications
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Author : United States. National Advisory Committee for Aeronautics
language : en
Publisher:
Release Date : 1954

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 1954 with Aeronautics categories.




Technical Note


Technical Note
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Author :
language : en
Publisher:
Release Date : 1956

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 1956 with Aeronautics categories.




Band Pass Shock And Vibration Absorbers For Application To Aircraft Landing Gear


Band Pass Shock And Vibration Absorbers For Application To Aircraft Landing Gear
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Author : Emanuel Schnitzer
language : en
Publisher:
Release Date : 1956

Band Pass Shock And Vibration Absorbers For Application To Aircraft Landing Gear written by Emanuel Schnitzer and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1956 with Airplanes categories.


A new class of frequency-selective shock absorbers called band-pass shock absorbers which were conceived as a means of overcoming some of the limitations of conventional shock absorbers is described. These shock absorber designs are introduced, special emphasis being given to their use in landing and taxiing problems of high-speed aircraft. For such aircraft operated on rough land or water runways, conventional oleo struts approach a rigid condition for bum[s with steep slopes and thereby develop and transmit severe shock loads to the aircraft fuselage. The operation of the band-pass shock absorbers in the reduction of loads in certain selected frequency ranges is described. Theoretical equations are derived and solutions are made for several cases for the purpose of comparing the low-pass and conventional shock-absorber actions. The results indicate that the band-pass shock absorbers should alleviate high-frequency or rapidly applied impact loads but should retain the characteristics of conventional oleo struts when taxiing and design landing loads are slowly applied. A number of variations in design are presented for low-pass shock absorbers and reference is made to double-acting band-pass vibration absorbers for other applications.



Applied Mechanics Reviews


Applied Mechanics Reviews
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Author :
language : en
Publisher:
Release Date : 1954

Applied Mechanics Reviews written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1954 with Mechanics, Applied categories.