THE EXTERNAL LOADS AND STRENGTH OF FLYING APPARATUSES
This book is dedicated to external loads having effect on a flight vehicle (aircraft and helicopter), and the durability of its construction. Basic attention in the book is allotted to actual problems of strength of contemporary flight vehicles: dynamic load, periods of service and strength of const...
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| creator | Gudkov,A. I Leshakov,P. S Ryakov,L. G |
| description | This book is dedicated to external loads having effect on a flight vehicle (aircraft and helicopter), and the durability of its construction. Basic attention in the book is allotted to actual problems of strength of contemporary flight vehicles: dynamic load, periods of service and strength of construction, strength during high speeds of flight, taking into account aerodynamic heating and others. Along with an account of theoretical questions in the book there are described experimental methods of investigating strength of construction. The book is designed for engineers connected with designing, tests, and exploitation of flight vehicles. At the same time, it can be used as a training aid for aviation students of higher educational institutions. (Author)
Edited machine trans. of mono. Vneshnie Nagruzki i Prochnost Letatelnykh Appartov, Moscow, 1963, 480p. Available copy will not permit fully legible reproduction. Reproduction will be made if requested by users of DDC. Copy is not available for public sale. |
| format | Report |
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Edited machine trans. of mono. Vneshnie Nagruzki i Prochnost Letatelnykh Appartov, Moscow, 1963, 480p. Available copy will not permit fully legible reproduction. Reproduction will be made if requested by users of DDC. Copy is not available for public sale.</description><language>eng</language><subject>AERODYNAMIC HEATING ; AERODYNAMIC LOADING ; AEROELASTICITY ; AIRCRAFT ; FATIGUE(MECHANICS) ; HELICOPTERS ; USSR</subject><creationdate>1965</creationdate><rights>APPROVED FOR PUBLIC RELEASE</rights><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,781,886,27569,27570</link.rule.ids><linktorsrc>$$Uhttps://apps.dtic.mil/sti/citations/AD0622400$$EView_record_in_DTIC$$FView_record_in_$$GDTIC$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Gudkov,A. I</creatorcontrib><creatorcontrib>Leshakov,P. S</creatorcontrib><creatorcontrib>Ryakov,L. G</creatorcontrib><creatorcontrib>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</creatorcontrib><title>THE EXTERNAL LOADS AND STRENGTH OF FLYING APPARATUSES</title><description>This book is dedicated to external loads having effect on a flight vehicle (aircraft and helicopter), and the durability of its construction. Basic attention in the book is allotted to actual problems of strength of contemporary flight vehicles: dynamic load, periods of service and strength of construction, strength during high speeds of flight, taking into account aerodynamic heating and others. Along with an account of theoretical questions in the book there are described experimental methods of investigating strength of construction. The book is designed for engineers connected with designing, tests, and exploitation of flight vehicles. At the same time, it can be used as a training aid for aviation students of higher educational institutions. (Author)
Edited machine trans. of mono. Vneshnie Nagruzki i Prochnost Letatelnykh Appartov, Moscow, 1963, 480p. Available copy will not permit fully legible reproduction. Reproduction will be made if requested by users of DDC. Copy is not available for public sale.</description><subject>AERODYNAMIC HEATING</subject><subject>AERODYNAMIC LOADING</subject><subject>AEROELASTICITY</subject><subject>AIRCRAFT</subject><subject>FATIGUE(MECHANICS)</subject><subject>HELICOPTERS</subject><subject>USSR</subject><fulltext>true</fulltext><rsrctype>report</rsrctype><creationdate>1965</creationdate><recordtype>report</recordtype><sourceid>1RU</sourceid><recordid>eNrjZDAN8XBVcI0IcQ3yc_RR8PF3dAlWcPRzUQgOCXL1cw_xUPB3U3DzifT0c1dwDAhwDHIMCQ12DeZhYE1LzClO5YXS3Awybq4hzh66KSWZyfHFJZl5qSXxji4GZkZGJgYGxgSkAVoWJJI</recordid><startdate>19650720</startdate><enddate>19650720</enddate><creator>Gudkov,A. I</creator><creator>Leshakov,P. S</creator><creator>Ryakov,L. G</creator><scope>1RU</scope><scope>BHM</scope></search><sort><creationdate>19650720</creationdate><title>THE EXTERNAL LOADS AND STRENGTH OF FLYING APPARATUSES</title><author>Gudkov,A. I ; Leshakov,P. S ; Ryakov,L. G</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-dtic_stinet_AD06224003</frbrgroupid><rsrctype>reports</rsrctype><prefilter>reports</prefilter><language>eng</language><creationdate>1965</creationdate><topic>AERODYNAMIC HEATING</topic><topic>AERODYNAMIC LOADING</topic><topic>AEROELASTICITY</topic><topic>AIRCRAFT</topic><topic>FATIGUE(MECHANICS)</topic><topic>HELICOPTERS</topic><topic>USSR</topic><toplevel>online_resources</toplevel><creatorcontrib>Gudkov,A. I</creatorcontrib><creatorcontrib>Leshakov,P. S</creatorcontrib><creatorcontrib>Ryakov,L. G</creatorcontrib><creatorcontrib>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</creatorcontrib><collection>DTIC Technical Reports</collection><collection>DTIC STINET</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Gudkov,A. I</au><au>Leshakov,P. S</au><au>Ryakov,L. G</au><aucorp>FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO</aucorp><format>book</format><genre>unknown</genre><ristype>RPRT</ristype><btitle>THE EXTERNAL LOADS AND STRENGTH OF FLYING APPARATUSES</btitle><date>1965-07-20</date><risdate>1965</risdate><abstract>This book is dedicated to external loads having effect on a flight vehicle (aircraft and helicopter), and the durability of its construction. Basic attention in the book is allotted to actual problems of strength of contemporary flight vehicles: dynamic load, periods of service and strength of construction, strength during high speeds of flight, taking into account aerodynamic heating and others. Along with an account of theoretical questions in the book there are described experimental methods of investigating strength of construction. The book is designed for engineers connected with designing, tests, and exploitation of flight vehicles. At the same time, it can be used as a training aid for aviation students of higher educational institutions. (Author)
Edited machine trans. of mono. Vneshnie Nagruzki i Prochnost Letatelnykh Appartov, Moscow, 1963, 480p. Available copy will not permit fully legible reproduction. Reproduction will be made if requested by users of DDC. Copy is not available for public sale.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| source | DTIC Technical Reports |
| subjects | AERODYNAMIC HEATING AERODYNAMIC LOADING AEROELASTICITY AIRCRAFT FATIGUE(MECHANICS) HELICOPTERS USSR |
| title | THE EXTERNAL LOADS AND STRENGTH OF FLYING APPARATUSES |
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