Cambered Wings

18 books
Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wingJohn W. Smith
⏱ 37m

Variable-camber systems integration and operational performance of the AFTI/F-111 mission adaptive wing

John W. Smith

199237 pp.
Estimated benefits of variable-geometry wing camber control for transport aircraftAlexander Bolonkin

Estimated benefits of variable-geometry wing camber control for transport aircraft

Alexander Bolonkin

1999No page data
Effect of camber on the trimmed lift capability of a close-coupled canard-wing configurationBlair B Gloss
⏱ 1h 31m

Effect of camber on the trimmed lift capability of a close-coupled canard-wing configuration

Blair B Gloss

197891 pp.
Delta wings with longitudinal camber at low speedR. K. Nangia
⏱ 18m

Delta wings with longitudinal camber at low speed

R. K. Nangia

197018 pp.
Wind tunnel tests on a variable camber wingA. MacKinnon
⏱ 3h 58m

Wind tunnel tests on a variable camber wing

A. MacKinnon

1993238 pp.
Camber effects on the non-linear lift of slender wings with sharp leading edgesLeonard Charles Squire
⏱ 18m

Camber effects on the non-linear lift of slender wings with sharp leading edges

Leonard Charles Squire

196718 pp.
In-flight transport performance optimizationGlenn B. Gilyard
⏱ 15m

In-flight transport performance optimization

Glenn B. Gilyard

199715 pp.
Delta wings with shock-free cross flowS. S. Sritharan

Delta wings with shock-free cross flow

S. S. Sritharan

1984No page data
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camberUnknown Author

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber

Unknown Author

1996No page data
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camberUnknown Author

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber

Unknown Author

1996No page data
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camberUnknown Author

Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber

Unknown Author

1996No page data
Surface-pressure and flow-visualization data at mach number 1.60 for three 65p0s delta wings varying in leading-edge radius and camberUnknown Author
⏱ 4h 22m

Surface-pressure and flow-visualization data at mach number 1.60 for three 65p0s delta wings varying in leading-edge radius and camber

Unknown Author

1996262 pp.
High-lift systems on commercial subsonic airlinersPeter K. C. Rudolph
⏱ 2h 35m

High-lift systems on commercial subsonic airliners

Peter K. C. Rudolph

1996155 pp.
Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbancesLisa J. Bjarke

Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances

Lisa J. Bjarke

1990No page data
Flight test of an adaptive configuration optimization system for transport aircraftGlenn B. Gilyard

Flight test of an adaptive configuration optimization system for transport aircraft

Glenn B. Gilyard

1999No page data
Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰M. Leroy Spearman

Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰

M. Leroy Spearman

1985No page data
A concept for adaptive performance optimization on commercial transport aircraftMichael R. Jackson

A concept for adaptive performance optimization on commercial transport aircraft

Michael R. Jackson

1995No page data
Euler technology assessment for preliminary aircraft designTodd R. Michal

Euler technology assessment for preliminary aircraft design

Todd R. Michal

1998No page data