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triangular wings

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View Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices By Kōichi Fujii

Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices

Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices

By Kōichi Fujii

View The natural flow wing-design concept By Richard M. Wood

The natural flow wing-design concept

The natural flow wing-design concept

By Richard M. Wood

View Some low-speed flutter characteristics of simple low-aspect-ration delta wing models By Robert V. Doggett

Some low-speed flutter characteristics of simple low-aspect-ration delta wing models

Some low-speed flutter characteristics of simple low-aspect-ration delta wing models

By Robert V. Doggett

View Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings By S. Naomi McMillin

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings

Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings

By S. Naomi McMillin

View High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers By Dhanvada M. Rao

High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers

High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers

By Dhanvada M. Rao

View Dual methods and approximation concepts in structural synthesis By Claude Fleury

Dual methods and approximation concepts in structural synthesis

Dual methods and approximation concepts in structural synthesis

By Claude Fleury

View The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps By Arthur C. Grantz

The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps

The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps

By Arthur C. Grantz

View Uniform approximation to the shock generated by thin, nonlifting wings of rectangular planform By Sanford S. Davis

Uniform approximation to the shock generated by thin, nonlifting wings of rectangular planform

Uniform approximation to the shock generated by thin, nonlifting wings of rectangular planform

By Sanford S. Davis

View Delta wings with shock-free cross flow By S. S. Sritharan

Delta wings with shock-free cross flow

Delta wings with shock-free cross flow

By S. S. Sritharan

View Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls By Donald Isaacs

Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls

Tests at subsonic and supersonic speeds on a slender cambered wing with fin, underwing engine nacelles and trailing-edge controls

By Donald Isaacs

View The Delta Wing By Alexander Lippisch

The Delta Wing

The Delta Wing

By Alexander Lippisch

View Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing By Kalpana Chawla

Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing

Numerical simulation of a powered-lift landing, tracking flow features using overset grids, and simulation of high lift devices on a fighter-lift-and-control wing

By Kalpana Chawla

View Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 By E. Ann Bare

Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2

Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2

By E. Ann Bare

View Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations By D. Brooke

Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations

Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations

By D. Brooke

View Numerical solutions of Navier-Stokes equations for a Butler wing By Jamshid S. Abolhassani

Numerical solutions of Navier-Stokes equations for a Butler wing

Numerical solutions of Navier-Stokes equations for a Butler wing

By Jamshid S. Abolhassani

View The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps By Arthur C Grantz

The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps

The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps

By Arthur C Grantz

View Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰ By H. F. Faery

Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰

Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60⁰

By H. F. Faery

View Development of aerodynamic prediction methods for irregular planform wings By David B. Benepe

Development of aerodynamic prediction methods for irregular planform wings

Development of aerodynamic prediction methods for irregular planform wings

By David B. Benepe

View Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow By Y. Y. Chan

Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow

Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow

By Y. Y. Chan

View The pressure distribution at zero lift on a slender delta wing at transonic speeds By Michael Charles Peter Firmin

The pressure distribution at zero lift on a slender delta wing at transonic speeds

The pressure distribution at zero lift on a slender delta wing at transonic speeds

By Michael Charles Peter Firmin

View Low-speed wind-tunnel experiments on a series of sharp-edged delta wings By P. B. Earnshaw

Low-speed wind-tunnel experiments on a series of sharp-edged delta wings

Low-speed wind-tunnel experiments on a series of sharp-edged delta wings

By P. B. Earnshaw

View Measurements of the effects of thickness on vortex breakdown position on a series of sharp-edged delta wings By P. B. Earnshaw

Measurements of the effects of thickness on vortex breakdown position on a series of sharp-edged delta wings

Measurements of the effects of thickness on vortex breakdown position on a series of sharp-edged delta wings

By P. B. Earnshaw

View Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung = By M. Beukenberg

Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung =

Aerodynamische Untersuchungen an Doppeldeltaflügeln bei unsymmetrischer Strömung =

By M. Beukenberg

View Delta wings with longitudinal camber at low speed By R. K. Nangia

Delta wings with longitudinal camber at low speed

Delta wings with longitudinal camber at low speed

By R. K. Nangia