Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 1 457mm span delta wing

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method /

Sleeman, William C.
Becht, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1949

This paper presents the results of the investigation of wing-alone and wing-fuselage combination emp...

Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel /

Naeseth, Rodger L.
Gainer, Thomas G.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1963

An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 2 1.15m span delta wing (effect of flap deflection angle and leading-edge radius)

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...

The performance of 60deg delta wings The effects of leading edge radius on vortex flaps and the wing

Hu, B.
Stollery, J
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1990

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9004) / BLDSC - Brit...

The performance of 60deg delta wings The effects of leading edge radius and vortex flaps

Hu, B.
Stollery, J
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1989

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9002) / BLDSC - Brit...

Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps

Rinoie, K.

January 1996

Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a r...

Development of Delta Wing Aerodynamics Research in Universiti Teknologi Malaysia Low Speed Wind Tunnel

Shabudin Mat
I. S. Ishak
Tholudin Mat Lazim
Shuhaimi Mansor
Mazuriah Said
Abdul Basid Abdul Rahman
Ahmad Shukeri Mohd. Kamaludim
Romain Brossay

July 2014

This paper presents wind tunnel experiment on two delta wing configurations which are differentiated...

Experimental studies of vortex flaps and vortex plates part 1 0.53m 60deg delta wing

Rinoie, K.
Stollery, J
Cranfield Inst. of Technology (United Kingdom). Coll. of Aeronautics

January 1991

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CA-R--9113) / BLDSC - Bri...

Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges

Peckham, D.H
Royal Aircraft Establishment, Bedford (United Kingdom)

January 1958

Recently declassifiedAvailable from British Library Document Supply Centre- DSC:7595.50(RAE-AERO--26...

Research Article Development of Delta Wing Aerodynamics Research in

Universiti Teknologi
Malaysia Low
Speed Wind Tunnel

September 2016

Aerodynamic improvement of a delta wing in combination with leading edge flaps

Tadateru Ishide
Mao Itazawa

November 2017

Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been report...

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

Grantz, Arthur C.
Langley Research Center.
Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept.

January 1984

"Prepared [at Virginia Polytechnic Institute and State University, Aerospace and Ocean Engineering D...

Low speed aerodynamic characteristics of non-slender delta wing at low angles of attack

Mohamed, Mohamed Ali
Afgan, Imran
Hefny Salim, Mohamed
Mohamed, Ibrahim K.

December 2022

This article was supported by the German Research Foundation (DFG) and the Open Access Publication F...

Effect of thickness-to-chord ratio on aerodynamics of non-slender delta wing

Ghazijahani, Mohammad Sharifi
Yavuz, Mehmet Metin

May 2019

The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with sweep ...

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method /

Sleeman, William C.
Becht, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1949

This paper presents the results of the investigation of wing-alone and wing-fuselage combination emp...

Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel /

Naeseth, Rodger L.
Gainer, Thomas G.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1963

An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 2 1.15m span delta wing (effect of flap deflection angle and leading-edge radius)

Rinoie, K.
College of Aeronautics, Cranfield (United Kingdom)

January 1996

SIGLEAvailable from British Library Document Supply Centre-DSC:3310.760(9612) / BLDSC - British Libr...

The performance of 60deg delta wings The effects of leading edge radius on vortex flaps and the wing

Hu, B.
Stollery, J
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1990

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9004) / BLDSC - Brit...

The performance of 60deg delta wings The effects of leading edge radius and vortex flaps

Hu, B.
Stollery, J
Cranfield Inst. of Tech., Bedford (United Kingdom). Coll. of Aeronautics

January 1989

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CAR--9002) / BLDSC - Brit...

Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps

Rinoie, K.

January 1996

Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a r...

Development of Delta Wing Aerodynamics Research in Universiti Teknologi Malaysia Low Speed Wind Tunnel

Shabudin Mat
I. S. Ishak
Tholudin Mat Lazim
Shuhaimi Mansor
Mazuriah Said
Abdul Basid Abdul Rahman
Ahmad Shukeri Mohd. Kamaludim
Romain Brossay

July 2014

This paper presents wind tunnel experiment on two delta wing configurations which are differentiated...

Experimental studies of vortex flaps and vortex plates part 1 0.53m 60deg delta wing

Rinoie, K.
Stollery, J
Cranfield Inst. of Technology (United Kingdom). Coll. of Aeronautics

January 1991

8.00Available from British Library Document Supply Centre- DSC:3310.76(CIT-CA-R--9113) / BLDSC - Bri...

Low-speed wind-tunnel tests on a series of uncambered slender pointed wings with sharp edges

Peckham, D.H
Royal Aircraft Establishment, Bedford (United Kingdom)

January 1958

Recently declassifiedAvailable from British Library Document Supply Centre- DSC:7595.50(RAE-AERO--26...

Research Article Development of Delta Wing Aerodynamics Research in

Universiti Teknologi
Malaysia Low
Speed Wind Tunnel

September 2016

Aerodynamic improvement of a delta wing in combination with leading edge flaps

Tadateru Ishide
Mao Itazawa

November 2017

Recently, various studies of micro air vehicle (MAV) and unmanned air vehicle (UAV) have been report...

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

Grantz, Arthur C.
Langley Research Center.
Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept.

January 1984

"Prepared [at Virginia Polytechnic Institute and State University, Aerospace and Ocean Engineering D...

Low speed aerodynamic characteristics of non-slender delta wing at low angles of attack

Mohamed, Mohamed Ali
Afgan, Imran
Hefny Salim, Mohamed
Mohamed, Ibrahim K.

December 2022

This article was supported by the German Research Foundation (DFG) and the Open Access Publication F...

Effect of thickness-to-chord ratio on aerodynamics of non-slender delta wing

Ghazijahani, Mohammad Sharifi
Yavuz, Mehmet Metin

May 2019

The effect of thickness-to-chord (t/C) ratio on aerodynamics of a non-slender delta wing with sweep ...

The effects of rounding the leading edges on the characteristics of separated flow past delta wings of low aspect ratio

Zakharovi, S
Royal Aerospace Establishment, Farnborough (United Kingdom)

January 1990

Report also known as RAE-Trans--2164Available from British Library Document Supply Centre- DSC:0678....

Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section. Transonic-bump method /

Sleeman, William C.
Becht, Robert E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1949

This paper presents the results of the investigation of wing-alone and wing-fuselage combination emp...

Low-speed investigation of the effects of wing sweep on the aerodynamic characteristics of parawings having equal-length leading edges and keel /

Naeseth, Rodger L.
Gainer, Thomas G.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1963

An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodyna...

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 1 457mm span delta wing

Abstract

Extracted data

Low speed aerodynamic characteristics of 60 degree rounded leading-edge delta wing with vortex flaps part 1 457mm span delta wing

Abstract

Extracted data

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