Static Tests

59 books
Static test induced loads verification beyond elastic limitV. Verderaime

Static test induced loads verification beyond elastic limit

V. Verderaime

1996No page data
Soprotivlenie zhelezobetonnykh staticheski neopredelimykh balok silovym vozdeĭstvii͡amL. R. Maili͡an
⏱ 2h 54m

Soprotivlenie zhelezobetonnykh staticheski neopredelimykh balok silovym vozdeĭstvii͡am

L. R. Maili͡an

1989174 pp.
Technical evaluation motor no. 5 (TEM-5)Unknown Author

Technical evaluation motor no. 5 (TEM-5)

Unknown Author

1990No page data
Space shuttle production verification motor-1 (PV-1) static fireDiane Garecht

Space shuttle production verification motor-1 (PV-1) static fire

Diane Garecht

1989No page data
Investigation of axial positioning for flexural compressorsPeter Riggle

Investigation of axial positioning for flexural compressors

Peter Riggle

1991No page data
Test load verification through strain data analysisV. Verderaime

Test load verification through strain data analysis

V. Verderaime

1995No page data
Final report for ETP-0403, Residual stress measurements after proof and flightUnknown Author

Final report for ETP-0403, Residual stress measurements after proof and flight

Unknown Author

1997No page data
Final report for ETP-0403, Residual stress measurements after proof and flightUnknown Author

Final report for ETP-0403, Residual stress measurements after proof and flight

Unknown Author

1997No page data
Final report for ETP-0403, Residual stress measurements after proof and flightUnknown Author

Final report for ETP-0403, Residual stress measurements after proof and flight

Unknown Author

1997No page data
QM-8 final performance evaluation reportLowell V. Nelsen

QM-8 final performance evaluation report

Lowell V. Nelsen

1989No page data
Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capabilityLinda S. Bangert

Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability

Linda S. Bangert

1989No page data
A user's guide to the Langley 16-foot transonic tunnel complexUnknown Author

A user's guide to the Langley 16-foot transonic tunnel complex

Unknown Author

1990No page data
Space shuttle flight support motor no. 1 (FSM-1) final test reportPhil D. Hughes

Space shuttle flight support motor no. 1 (FSM-1) final test report

Phil D. Hughes

1990No page data
Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle conceptDavid J. Wing

Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept

David J. Wing

1994No page data
Analysis of static contact in laminated composite plates using damage mechanicsAllen, David H.

Analysis of static contact in laminated composite plates using damage mechanics

Allen, David H.

1995No page data
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzlesMary L. Mason
⏱ 3h 36m

Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles

Mary L. Mason

1985216 pp.
Advanced manufacturing development of a composite empennage component for L-1011 aircraft.Unknown Author
⏱ 1h 38m

Advanced manufacturing development of a composite empennage component for L-1011 aircraft.

Unknown Author

198498 pp.
Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplaneDonald L. Hughes

Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane

Donald L. Hughes

1985No page data
Static strain and vibration characteristics of a metal semimonocoque helicopter tail cone of moderate sizeRichard L. Bielawa

Static strain and vibration characteristics of a metal semimonocoque helicopter tail cone of moderate size

Richard L. Bielawa

1991No page data
Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capabilityGeorge T. Carson

Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability

George T. Carson

1991No page data
← PreviousPage 2 of 3Next →