Helicopter structures : a review of loads, fatigue design techniques and usage monitoring /

This report is a review of traditional practice with respect to helicopter structural integrity. Aspects covered are: significant fatigue loads for the airframe and rotor system, the methods used in the fatigue design of current and previous generation rotorcraft, fatigue test requirements, and heal...

Full description

Saved in:
Bibliographic Details
Main Author: Lombardo, D. C.
Corporate Author: Aeronautical Research Laboratory (Australia)
Format: Book
Language:English
Published: Fisherman's Bend, Vic. : Dept. of Defence, Defence Science and Technology Organisation, Aeronautical Research Laboratory, c1993.
Series:Technical report (Aeronautical Research Laboratory (Australia)) ; 15.
Subjects:
LEADER 02032cam a2200397 a 4500
001 c000259573
003 CARM
005 20070502133521.0
008 930921s1993 vraa bs f000 0 eng d
019 1 |a 10367989  |5 LACONCORD2021 
024 0 |a AR-007-137 
035 |a (OCoLC)38339262  |5 LACONCORD2021 
040 |a NNCU:A  |b eng  |c NNCU:A  |d ANL 
042 |a anuc 
043 |a u-at--- 
050 1 4 |a TL716  |b .L65 1993 
082 0 4 |a 629.13431  |2 20 
100 1 |a Lombardo, D. C. 
245 1 0 |a Helicopter structures :  |b a review of loads, fatigue design techniques and usage monitoring /  |c by D.C. Lombardo. 
260 |a Fisherman's Bend, Vic. :  |b Dept. of Defence, Defence Science and Technology Organisation, Aeronautical Research Laboratory,  |c c1993. 
300 |a 60 leaves :  |b ill., (1 col.) ;  |c 30 cm. 
490 1 |a Technical report / Aeronautical Research Laboratory (Australia) ;  |v 15 
500 |a "A review of traditional practice with respect to helicopter structural integrity." 
500 |a "AR-007-137" -- at head of t.p. 
500 |a Includes statistical tables. 
504 |a Bibliography: leaves 49-55. 
520 0 |a This report is a review of traditional practice with respect to helicopter structural integrity. Aspects covered are: significant fatigue loads for the airframe and rotor system, the methods used in the fatigue design of current and previous generation rotorcraft, fatigue test requirements, and health and usage monitoring methods. 
540 |a Commonwealth of Australia 1993. 
650 0 |a Helicopters. 
650 0 |a Airframes  |x Fatigue  |x Measurement. 
650 0 |a Airframes  |x Fatigue  |x Research  |z Australia. 
710 2 |a Aeronautical Research Laboratory (Australia) 
830 0 |a Technical report (Aeronautical Research Laboratory (Australia)) ;  |v 15. 
852 8 |b CARM  |h A1:AP21F0  |i F02043  |p 0342544  |f BK 
999 f f |i 8c78a5f0-77ae-5c20-bbf4-4e7a3cabbfff  |s 11f4b104-152b-588c-9a2e-e527589629f9 
952 f f |p Can circulate  |a CAVAL  |b CAVAL  |c CAVAL  |d CARM 1 Store  |e F02043  |f A1:AP21F0  |h Other scheme  |i book  |m 0342544