by grubb » Sun Mar 08, 2015 10:32 pm
Hi,
I can't seem to PM you yet Sooty655, maybe it's because I haven't posted enough yet.
I have managed to get to Kew and photograph the file you mentioned, I'm due to go back and view some of these:
Metal fatigue in aircraft: reports
Reference: BT 248/301
Description:
Metal fatigue in aircraft: reports
Date: 1952-1961
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Reference: AIR 20/10764
Description:
Vulcan aircraft: wind tunnel test results
Date: 1954-1957
Held by: The National Archives, Kew
Former reference in its original department VB/203/8 (Part 2)
Legal status: Public Record
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Jaguar aircraft: fatigue life
Reference: AVIA 65/1752
Description:
Jaguar aircraft: fatigue life
Date: 1965-1972
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Cumulative damage theory of metal fatigue
Reference: DSIR 23/17248
Description:
Cumulative damage theory of metal fatigue
Date: 1948
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RAW MATERIALS (Code 42): Metal fatigue detection prior to development of cracks in light...
Reference: AVIA 15/3360
Description:
RAW MATERIALS (Code 42): Metal fatigue detection prior to development of cracks in light alloy: reports
Date: 1945-1954
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Literature review on cyclic stress induced metal fatigue(NGTE M320)
Reference: DSIR 23/26312
Description:
Literature review on cyclic stress induced metal fatigue(NGTE M320)
Date: 1958
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Fatigue of metals, especially aluminium
Reference: DSIR 23/31185
Description:
Fatigue of metals, especially aluminium
Date: 1963
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Statistical nature of fatigue of metals
Reference: DSIR 23/22810
Description:
Statistical nature of fatigue of metals
Date: 1954
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Fatigue characteristics of a metal wing
Reference: DSIR 23/23611
Description:
Fatigue characteristics of a metal wing
Date: 1955
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Basic Properties of Metals Committee: some metallographic changes produced by fatiguing aluminium alloys
Reference: SUPP 19/1263
Description:
Basic Properties of Metals Committee: some metallographic changes produced by fatiguing aluminium alloys
Note: With photographs
Date: 1954 Jan 01-1954 Dec 31
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The British Non Ferrous Metals Research Association: fatigue properties of a magnesium - ½% zirconium alloy
Reference: AB 7/12151
Description:
The British Non Ferrous Metals Research Association: fatigue properties of a magnesium - ½% zirconium alloy
Date: 1961 Nov
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The fatigue properties of three aluminium alloys and a mild steel with respect to structural applications D S Higgs, J McKeown and A R Goreham
Date: 1960 Oct
Reference: AB 7/9707
Description:
The fatigue properties of three aluminium alloys and a mild steel with respect to structural applications D S Higgs, J McKeown and A R Goreham
Date: 1960 Oct
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A.V Roe & Co: design and manufacture of Vulcan aircraft
Reference: AVIA 53/18
Description:
A.V Roe & Co: design and manufacture of Vulcan aircraft
Date: 1947-1954
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Production of Vulcan mk.l aircraft by AV Roe Ltd: policy
Reference: AVIA 65/215
Description:
Production of Vulcan mk.l aircraft by AV Roe Ltd: policy
Date: 1952-1956
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Pitch derivatives for Avro Vulcan and DH 108 wings
Reference: DSIR 23/21323
Description:
Pitch derivatives for Avro Vulcan and DH 108 wings
Date: 1952
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Vulcan B Mks 1 and 2: alterations on structural strength. Includes 16 photographs...
Reference: AVIA 65/1279
Description:
Vulcan B Mks 1 and 2: alterations on structural strength.
Includes 16 photographs depicting: (1) Avro Vulcan: wing vulnerability against small shell explosions; tests (2) Delta-Wing Bomber (Vulcan) MK1 and MK2 models (3) Vulcan MK1 and MK2: oil flow patterns on wings (4) X-ray tube used to locate cracks in stringer brackets at front and rear. Dated 1956.
Date: 1957-1959
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Strength in comparison and tension of an aluminium alloy extruded angle to specification DTD 683A
Reference: AVIA 6/21145
Description:
Strength in comparison and tension of an aluminium alloy extruded angle to specification DTD 683A
Date: 1958