Delta Wings

66 books
Study of lee-side flows over conically cambered delta wings at supersonic speedsRichard M. Wood

Study of lee-side flows over conically cambered delta wings at supersonic speeds

Richard M. Wood

1987No page data
The performance of 60 deg delta wings: the effects of leading edge radius and vortex flapsB. K. Hu
⏱ 23m

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

B. K. Hu

198923 pp.
Application of the vortex cloud method to slender, flapped delta wingsSejong Oh
⏱ 1h 24m

Application of the vortex cloud method to slender, flapped delta wings

Sejong Oh

198784 pp.
The performance of 60 degree delta wings: the effects of leading edge radius on vortex flaps and the wingB. K. Hu
⏱ 34m

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

B. K. Hu

199034 pp.
An analysis of conical augmentor/delta wing integrationDomingo A. Tavella
⏱ 22m

An analysis of conical augmentor/delta wing integration

Domingo A. Tavella

198722 pp.
Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planformLong P. Yip
⏱ 32m

Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform

Long P. Yip

199032 pp.
Pressure measurements on a thick cambered and twisted 58ʻ́Julio Chu

Pressure measurements on a thick cambered and twisted 58ʻ́

Julio Chu

1987No page data
The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attackTorsten Berglind
⏱ 12m

The influence of the leading edge geometry on the wave drag for a 65 degree delta wing at low supersonic speed and small angles of attack

Torsten Berglind

198812 pp.
Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental dataKrishnaswami Yegna Narayan
⏱ 1h 4m

Transonic and supersonic flow past a 65 degree delta wing with rounded leading edges - analysis of experimental data

Krishnaswami Yegna Narayan

198864 pp.
The aerodynamics of delta wings of elliptical cross-section with separated flowNikos J. Mourtos
⏱ 53m

The aerodynamics of delta wings of elliptical cross-section with separated flow

Nikos J. Mourtos

198553 pp.
Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speedsJulio Chu
⏱ 3h 58m

Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds

Julio Chu

1987238 pp.
An exact theory of supersonic flow around a delta wingL. R. Fowell
⏱ 1h 32m

An exact theory of supersonic flow around a delta wing

L. R. Fowell

195592 pp.
Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speedsPeter F. Covell
⏱ 2h 3m

Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds

Peter F. Covell

1987123 pp.
Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplaneJay M. Brandon
⏱ 35m

Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane

Jay M. Brandon

198735 pp.
Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wingGary E. Erickson
⏱ 2h 47m

Effects of forebody strakes and Mach number on overall aerodynamic characteristics of configuration with 55 deg cropped delta wing

Gary E. Erickson

1992167 pp.
A visualisation study of the vortex flow around double-delta wingsD. H. Thompson
⏱ 12m

A visualisation study of the vortex flow around double-delta wings

D. H. Thompson

198512 pp.
Numerical solutions of Navier-Stokes equations for a Butler wingSurendra N. Tiwari
⏱ 44m

Numerical solutions of Navier-Stokes equations for a Butler wing

Surendra N. Tiwari

198544 pp.
Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysisS. N. Seshadri
⏱ 1h 3m

Evaluation of LDA 3-component velocity data on a 65 [degree] delta wing at M=0.85 and first results of an analysis

S. N. Seshadri

198963 pp.
Experimental studies of a delta wing with leading edge flapsChyang S. Lee
⏱ 35m

Experimental studies of a delta wing with leading edge flaps

Chyang S. Lee

198735 pp.
Controlled vortical flow on delta wings through unsteady leading edge blowingK. T. Lee

Controlled vortical flow on delta wings through unsteady leading edge blowing

K. T. Lee

1990No page data
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