Tomeki

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ground simulators

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View Wind-tunnel test of an articulated helicopter rotor model with several tip shapes By John D. Berry

Wind-tunnel test of an articulated helicopter rotor model with several tip shapes

Wind-tunnel test of an articulated helicopter rotor model with several tip shapes

By John D. Berry

View Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê By William Mulcay

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê

By William Mulcay

View The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models By William A. Scott

The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models

The preliminary checkout, evaluation and calibration of a 3-component force measurement system for calibrating propulsion simulators for wind tunnel models

By William A. Scott

View Performance testing of a main rotor system for a utility helicopter at 1/4 scale By John D. Berry

Performance testing of a main rotor system for a utility helicopter at 1/4 scale

Performance testing of a main rotor system for a utility helicopter at 1/4 scale

By John D. Berry

View Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG] By William Mulcay

Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]

Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8t̊o 90[ANG]

By William Mulcay

View Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes By John D Berry

Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes

Wind-tunnel test of an articlulated helicopter rotor model with several tip shapes

By John D Berry

View Applications and requirements for real-time simulators in ground-test facilities By Dale J. Arpasi

Applications and requirements for real-time simulators in ground-test facilities

Applications and requirements for real-time simulators in ground-test facilities

By Dale J. Arpasi

View Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊ By William Mulcay

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊

Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊

By William Mulcay

View Advanced hypersonic test facilities By Frank K. Lu
Cover of Advanced hypersonic test facilities by frank k. lu

Advanced hypersonic test facilities

By Frank K. Lu

View Wind tunnel simulation and field measurements of flow over a coastal headland By Roger West Brownlow

Wind tunnel simulation and field measurements of flow over a coastal headland

Wind tunnel simulation and field measurements of flow over a coastal headland

By Roger West Brownlow

View Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests By Delma C Freeman

Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests

Comparison of space shuttle orbiter low-speed static stability and control derivatives obtained from wind-tunnel and approach and landing flight tests

By Delma C Freeman

View Performance testing of a main rotor system for a utility helicopter at 1/4 scale By John D Berry

Performance testing of a main rotor system for a utility helicopter at 1/4 scale

Performance testing of a main rotor system for a utility helicopter at 1/4 scale

By John D Berry

View Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG] By William Mulcay

Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG]

Rotary balance data for a single-engine agricultural airplane configuration for an angle-of-attack range of 8êto 90[ANG]

By William Mulcay

View A moving-belt rig for ground simulation in low-speed wind tunnels By S. F. J. Butler

A moving-belt rig for ground simulation in low-speed wind tunnels

A moving-belt rig for ground simulation in low-speed wind tunnels

By S. F. J. Butler

View Wind tunnel measurements in the wakes of structures By H. G. C. Woo

Wind tunnel measurements in the wakes of structures

Wind tunnel measurements in the wakes of structures

By H. G. C. Woo

View Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation By G. Schulz

Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation

Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation

By G. Schulz

View A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel By Pierce L Lawing

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel

By Pierce L Lawing