Swept Wings

88 books
Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wingPaul L. Coe
⏱ 1h 7m

Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing

Paul L. Coe

198367 pp.
Leading-edge deflection optimization for a highly swept arrow-wing configurationPaul L Coe
⏱ 56m

Leading-edge deflection optimization for a highly swept arrow-wing configuration

Paul L Coe

198056 pp.
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 inletColin S. Bidwell

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

Colin S. Bidwell

1995No page data
AGARD standard aeroelastic configurations for dynamic responseE. Carson Yates
⏱ 1h 14m

AGARD standard aeroelastic configurations for dynamic response

E. Carson Yates

198774 pp.
Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wingSamuel J. Scott

Effects of leading-edge devices on the low-speed aerodynamic characteristics of a highly-swept arrow-wing

Samuel J. Scott

1985No page data
Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slipRaymond D. Whipple
⏱ 4h 46m

Low-speed aerodynamic characteristics of a 1/8-scale X-29A airplane model at high angles of attack and side slip

Raymond D. Whipple

1986286 pp.
Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow controlVenkit Iyer
⏱ 1h 30m

Three-dimensional boundary-layer program (BL3D) for swept subsonic or supersonic wings with application to laminar flow control

Venkit Iyer

199390 pp.
Flight tests on the Short SB5 with 60 degrees sweepback and low tailplaneK. J. Staples

Flight tests on the Short SB5 with 60 degrees sweepback and low tailplane

K. J. Staples

1969No page data
The estimation of the loading on swept wings with extending chord flaps at subsonic speedsJ. McKie
⏱ 30m

The estimation of the loading on swept wings with extending chord flaps at subsonic speeds

J. McKie

197030 pp.
The subcritical response and flutter of a swept-wing modelC. A. K. Irwin
⏱ 31m

The subcritical response and flutter of a swept-wing model

C. A. K. Irwin

196831 pp.
experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinationsLangley Aeronautical Laboratory
⏱ 36m

experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations

Langley Aeronautical Laboratory

195536 pp.
Analysis of iced wingsUnknown Author

Analysis of iced wings

Unknown Author

1992No page data
Crossflow stability and transition experiments in a swept-wing flowJ. Ray Dagenhart

Crossflow stability and transition experiments in a swept-wing flow

J. Ray Dagenhart

1992No page data
A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wingsShawn H. Woodson

A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings

Shawn H. Woodson

1988No page data
A brief description of the Jameson-Caughey NYU transonic swept-wing computer program - FLO 22Antony Jameson
⏱ 32m

A brief description of the Jameson-Caughey NYU transonic swept-wing computer program - FLO 22

Antony Jameson

197632 pp.
Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wingChristine M. Darden
⏱ 1h 27m

Effect of milling machine roughness and wing dihedral on the supersonic aerodynamic characteristics of a highly swept wing

Christine M. Darden

198987 pp.
Nonlinear wave interactions in swept wing flowsNabil M. El-Hady

Nonlinear wave interactions in swept wing flows

Nabil M. El-Hady

1988No page data
Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wingDhanvada M. Rao

Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing

Dhanvada M. Rao

1987No page data
Detailed flow-field measurements over a 75⁰ swept delta wingScott O. Kjelgaard

Detailed flow-field measurements over a 75⁰ swept delta wing

Scott O. Kjelgaard

1990No page data
A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall regionEdward C. Polhamus

A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall region

Edward C. Polhamus

1996No page data
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