1-17 of 17 Books
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
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
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
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
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
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
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
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

Advanced hypersonic test facilities
By Frank K. Lu
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
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
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
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
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
Wind tunnel measurements in the wakes of structures
Wind tunnel measurements in the wakes of structures
By H. G. C. Woo
Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation
Die Verdrängungskorrekturen in Unterschallwindkanälen bei sperrigen Modellen und mit Bodensimulation
By G. Schulz
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