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Published: 01 July 2009
Fig. 10.2 Comparison of fatigue regimes encountered in the Space Shuttle Main Engines (SSMEs) and that encountered in aeronautical gas turbine engines More
Image
Published: 01 October 2005
Fig. 2.21 A non-return valve that can be fitted incorrectly because of its design. Source: Ref 12 . With kind permission of Royal Aeronautical Society More
Image
Published: 01 June 1988
Fig. 2.6 Reference depth for common materials as a function of frequency. From A. F. Leatherman and D. E. Stutz, “Induction Heating Advances: Application to 5800 F,” NASA Report SP-5071, National Aeronautics and Space Administration, Washington, 1969 ( Ref 4 ) More
Image
Published: 01 June 1988
Fig. 2.10 Relationship between relative efficiency and critical frequency. From A. F. Leatherman and D. E. Stutz, “Induction Heating Advances: Application to 5800 F,” NASA Report SP-5071, National Aeronautics and Space Administration, Washington, 1969 ( Ref 4 ) More
Image
Published: 01 June 1988
Fig. 2.9 Critical frequency for efficient induction heating of several materials as a function of bar size. From A. F. Leatherman and D. E. Stutz, “Induction Heating Advances: Application to 5800 F,” NASA Report SP-5071, National Aeronautics and Space Administration, Washington, 1969 ( Ref 4 ) More
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Published: 01 October 2012
Fig. 2.45 Friction stir weld process development tool at the Marshall Space Flight Center (MSFC) shown with an 8.2 m (27 ft) diameter barrel segment of the 2195 aluminum-lithium Space Shuttle. National Aeronautics and Space Administration (NASA) Michoud Assembly Facility in New Orleans More
Image
Published: 01 November 2011
Fig. 6.21 Friction stir weld process development tool at the Marshall Space Flight Center shown with an 8.2 m (27 ft) diameter barrel segment of the 2195 Al-Li external tank for the Space Shuttle at the National Aeronautics and Space Administration (NASA) Michoud Assembly Facility in New More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2010
DOI: 10.31399/asm.tb.hss.t52790229
EISBN: 978-1-62708-356-0
... that reduce section thickness of the stainless steel frame without sacrificing structural integrity. (It is interesting to consider that Albert Dean, the young aeronautical engineer, had designed the Budd trains within only 15% of the ideal weight by using mathematical equations and a slide rule...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 1988
DOI: 10.31399/asm.tb.eihdca.t65220009
EISBN: 978-1-62708-341-6
..., National Aeronautics and Space Administration, Washington, 1969 ( Ref 4 ) Fig. 2.7 Reference (skin) depth for magnetic steel as a function of power density and frequency. From G. H. Brown, C. N. Hoyler, and R. A. Bierwirth, Theory and Application of Radio Frequency Heating , Van Nostrand, New...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 October 2005
DOI: 10.31399/asm.tb.faesmch.t51270045
EISBN: 978-1-62708-301-0
... structures as well. References References 1. Tardif H.P. and Sterling T.S. , J. Forensic Sci. , Vol 12 ( No. 3 ), 1967 , p 247 2. Newton E. , Can. Aeronaut. Space J. , Vol 14 , 1968 , p 385 3. Tardif H.P. and Sterling T.S. , Can. Aeronaut. Space J...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 1983
DOI: 10.31399/asm.tb.mlt.t62860343
EISBN: 978-1-62708-348-5
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060231
EISBN: 978-1-62708-343-0
.... It then describes the types of damage observed in engine components and the methods used to mitigate problems. It also discusses the results of analyses that led to changes in design or approach and examines fatigue-related issues in turbine engines used in commercial aircraft. aeronautical gas turbine...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2003
DOI: 10.31399/asm.tb.cfap.9781627082815
EISBN: 978-1-62708-281-5
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.stg2.t61280365
EISBN: 978-1-62708-267-9
... al. , Machining and Grinding of Nickel- and Cobalt-Base Alloys , Report TM X-53446, National Aeronautics and Space Administration , 1966 • Vagi J. et al. , Joining of Nickel and Nickel-Base Alloys , Report TM X-53447, National Aeronautics and Space Administration , 1966...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2003
DOI: 10.31399/asm.tb.cfap.t69780433
EISBN: 978-1-62708-281-5
... ow rate melt index methyl methacrylate metaphenylene diamine modi ed polyphenylene ether modi ed polyphenylene oxide molecular weight molecular-weight distribution number of cycles number of cycles to failure National Aeronautics and Space Administration National Bureau of Standards National Fire...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060083
EISBN: 978-1-62708-343-0
... Engineers (ASME) Boiler and Pressure Vessel Code. Detailed creep-fatigue test results with testing durations approaching 1 year were generated for three pressure vessel and piping steels in various heat treated conditions. These were made available to Saltsman of the National Aeronautics and Space...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.scm.t52870401
EISBN: 978-1-62708-314-0
... Memorandum 113116/Rev 1, National Aeronautics and Space Administration , July 1998 9. Bowles K.J. , McCorkle L. , and Ingrahm L. , “ Comparison of Graphite Fabric Reinforced PMR-15 and Avimid N Composites After Long Term Isothermal Aging at Various Temperatures ”, NASA/TM-1998...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2010
DOI: 10.31399/asm.tb.hss.t52790123
EISBN: 978-1-62708-356-0
... aeronautical engineer from Massachusetts Institute of Technology, comprised the team assigned to design and build what would be called the Budd-Micheline experimental train. Instead of attempting to emulate the traditional boxlike design of passenger cars, replacing the structural steel with high-strength...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2010
DOI: 10.31399/asm.tb.omfrc.t53030237
EISBN: 978-1-62708-349-2
...-matrix composite specimen shown in Fig. 14.5 ( a and b ) is typical for the polymer composites that flew on the leading edge of the National Aeronautics and Space Administration’s (NASA’s) Long-Duration Exposure Facility (LDEF). The material specimens and systems on board this 60-ton, experiment-laden...
Book Chapter

Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2006
DOI: 10.31399/asm.tb.fdsm.t69870105
EISBN: 978-1-62708-344-7
... and Materials , 2000 , p 369 – 381 10.1520/STP13515S 5.2 Ellis J.R. and Abdul-Aziz A. , “Specimen Designs for Testing Advanced Aeropropulsion Materials under In-Plane Biaxial Loading,” NASA/TM-2003-212090 , National Aeronautics and Space Administration , January 2003 5.3...