1-24 of 33 Books
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil
By Cuyler W. Brooks
Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip
By Raymond D. Whipple
Swept-wing receptivity studies using distributed roughness
Swept-wing receptivity studies using distributed roughness
By W. S. Saric
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle
By Stephen W. D. Wolf
Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control
Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control
By Venkit Iyer
Distributed-roughness effects on stability and transition in swept-wing boundary layers
Distributed-roughness effects on stability and transition in swept-wing boundary layers
By Ruben B. Carrillo
Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data
By R. C. Potter
Navier-Stokes simulation of the crossflow instability in swept-wing flows
Navier-Stokes simulation of the crossflow instability in swept-wing flows
By Helen L. Reed
Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
By Gregory M. Catlin
A swept wing panel in a low speed flexible walled test section
A swept wing panel in a low speed flexible walled test section
By M. J. Goodyer
A spectrally accurate boundary-layer code for infinite swept wings
A spectrally accurate boundary-layer code for infinite swept wings
By C. David Pruett
Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing
Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing
By Dhanvada M. Rao
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing
By Sheryll Goecke Powers
Study of potential aerodynamic benefits from spanwise blowing at wingtip
Study of potential aerodynamic benefits from spanwise blowing at wingtip
By Raymond E. Mineck
Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing
Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing
By Samuel J. Scott
Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
By Colin S. Bidwell
Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
By W. S. Saric
A brief description of the Jameson-Caughey NYU transonic swept-wing computer program - FLO 22
A brief description of the Jameson-Caughey NYU transonic swept-wing computer program - FLO 22
By Antony Jameson
Vortex instabilities in 3D boundary layers
Vortex instabilities in 3D boundary layers
By Andrew P. Bassom
Physical mechanisms of glaze ice scallop formations on swept wings
Physical mechanisms of glaze ice scallop formations on swept wings
By Mario Vargas
Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
Unsteady, transonic flow around delta wings undergoing coupled and natural modes response
By Margaret Anne Menzies
AGARD standard aeroelastic configurations for dynamic response: I - Wing 445.6
AGARD standard aeroelastic configurations for dynamic response: I - Wing 445.6
By E. Carson Yates
Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing
Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing
By Christine M. Darden
Natural laminar flow flight experiments on a swept wing business jet
Natural laminar flow flight experiments on a swept wing business jet
By R. A. Rozendaal