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Delta
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keywords:(Delta)
Yaw-Control Spoiler Design Using Design of Experiments Based Wind Tunnel Testing
Yaw Angle Effect on Flow Structure over the Nonslender Diamond Wing
Wind Tunnel Pressure Signatures for a 0.0041-Scale Model of the Space Shuttle Orbiter
Wind-Tunnel Investigation of the Development of Lift on Wings in Accelerated Longitudinal Motion
Wind-Tunnel Investigation at a Mach Number of 1.53 of an Airplane with a Triangular Wing
Vortical Structures over a Generic Tailless Chined Forebody–Delta Wing
Vortex structures for flow over a delta wing with sinusoidal leading edge
Vortex Signature Identification in Surface Pressure Distributions Using Crease Detection Techniques
Vortex-Flow Manipulation on a Generic Delta-Wing Configuration
Vortex flow hypothesis for a yawed rotor blade in reverse flow*
Vortex flow and lift generation of a non-slender reverse delta wing
Vortex flow and lift generation of a non-slender reverse delta wing
Voice encoding for the Space Shuttle using adaptive delta modulation
Visualisation Study of the Vortex Flow Around Double-Delta Wings
Verification of Takeoff Performance Predictions for the Xb-70 Airplane
Vehicular Intercommunications System
Vehicle Test Report Fmvss 210: 1968 Oldsmobile delta
Vehicle Test Report Fmvss 207: 1968 Oldsmobile delta 88 Serial Number 366878C-113437
Vehicle Test Report Fmvss 110: 1968 Oldsmobile delta Serial Number 366878C-113437
Vehicle Test Report Fmvss 105: 1968 Oldsmobile delta 88
Vehicles Frontal Impact Analysis Using Computer Simulation and Crash Test
Vector Wave Equation of Aeroacoustics and Acoustic Velocity Formulations for Quadrupole Source
Vector Aeroacoustics for Uniform Mean Flow: Acoustic Velocity and Vortical Velocity
Vector Aeroacoustics for a Uniform Mean Flow: Acoustic Intensity and Acoustic Power
Validation of a Jet–Surface Interaction Noise Model in Flight
Utility of Space Transportation System to Space Communication Community
US Naval Forces, Vietnam Monthly Historical Summary for May 1966
U.S. Naval Forces, Vietnam Monthly Historical Summary for July 1969
Upstream Vortex Effects on Turbine Blade Platform Film Cooling With Typical Purge Flow