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Cover image for Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests

Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests

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Cover image for Development of a robust static punch experiment for screening unprocessed ultra-high molecular weight polyethylene (UHMWPE) unidirectional cross-ply material

Development of a robust static punch experiment for screening unprocessed ultra-high molecular weight polyethylene (UHMWPE) unidirectional cross-ply material

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Cover image for Report of static test on J. V. Martin shock-absorbing wheels with Curtiss JN4 chassis (Airplane Section, S. & A. Branch).

Report of static test on J. V. Martin shock-absorbing wheels with Curtiss JN4 chassis (Airplane Section, S. & A. Branch).

  • 1921
  • Format: Microform
Location Call # Status
Joyner - Microforms B300 CIS US EXEC MF W87.11-2.254 ✔ Available
Cover image for A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations

A transonic wind-tunnel investigation of the static longitudinal and lateral aerodynamic characteristics of a proposed hypersonic glider with several booster configurations

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Cover image for 650-2017 - IEEE Standard for Qualification of Class 1E Static Battery Chargers, Inverters, and Uninterruptible Power Supply Systems for Nuclear Power Generating Stations

650-2017 - IEEE Standard for Qualification of Class 1E Static Battery Chargers, Inverters, and Uninterruptible Power Supply Systems for Nuclear Power Generating Stations

  • 2018
  • Format: Electronic
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Cover image for Evaluation of a flow direction probe and a pilot-static probe on the F-14 airplane at high angles of attack and sideslip

Evaluation of a flow direction probe and a pilot-static probe on the F-14 airplane at high angles of attack and sideslip

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Cover image for Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01

Static stability and control characteristics of an airplane model with tail surfaces outboard of the wing tips at a mach number of 2.01

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Cover image for The philosophical works of the Honourable Robert Boyle Esq; abridged, methodized, and disposed under the general heads of physics, statics, pneumatics, ... By Peter Shaw, M.D.

The philosophical works of the Honourable Robert Boyle Esq; abridged, methodized, and disposed under the general heads of physics, statics, pneumatics, ... By Peter Shaw, M.D.

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Cover image for Discussion of stress analysis of airplane wing cellule of multi-spar type of wing construction, with special reference to loading condition of standard static test

Discussion of stress analysis of airplane wing cellule of multi-spar type of wing construction, with special reference to loading condition of standard static test

  • 1920
  • Format: Microform
Location Call # Status
Joyner - Microforms B300 CIS US EXEC MF W87.11-2.52 ✔ Available
Cover image for Pleasure with profit

Pleasure with profit

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