1-24 of 48 Books
Study of lee-side flows over conically cambered delta wings at supersonic speeds
Study of lee-side flows over conically cambered delta wings at supersonic speeds
By Richard M. Wood
Transonic Navier-Stokes calculations about a 65⁰ delta wing
Transonic Navier-Stokes calculations about a 65⁰ delta wing
By W. Kelly Londenberg
Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings
By Ken Craig
Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
Three-dimensional aerodynamic shape optimization using discrete sensitivity analysis
By Gregory Wayne Burgreen
Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
By Long P. Yip
An exact theory of supersonic flow around a delta wing
An exact theory of supersonic flow around a delta wing
By L. R. Fowell
Delta wings with shock-free cross flow
Delta wings with shock-free cross flow
By S. S. Sritharan
Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
Vapor-screen flow-visualization experiments in the NASA Langley 0.3-m transonic cryogenic tunnel
By Gregory V. Selby
Lee-side flow over delta wings at supersonic speeds
Lee-side flow over delta wings at supersonic speeds
By David S. Miller
Numerical solutions of Navier-Stokes equations for a Butler wing
Numerical solutions of Navier-Stokes equations for a Butler wing
By Jamshid S. Abolhassani
Detailed flow-field measurements over a 75⁰ swept delta wing
Detailed flow-field measurements over a 75⁰ swept delta wing
By Scott O. Kjelgaard
Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
Delta wing vortex manipulation using pulsed and steady blowing during ramp pitching
By J. Moreira
The art of sharp-leading-edged delta wings with blowing
The art of sharp-leading-edged delta wings with blowing
By D. A. Tavella
Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
By Osama A. Kandil
Theoretical and experimental investigation of vortex breakdown
Theoretical and experimental investigation of vortex breakdown
By E. Krause
On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings
On the swelling and break down of rolled up vortex sheets in inviscid flows around slender delta wings
By A. Das
Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations
By Robert M. Bennett
The aerodynamics of delta wings of elliptical cross-section with separated flow
The aerodynamics of delta wings of elliptical cross-section with separated flow
By Nikos J. Mourtos
Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
By Roger A. Lepsch
The lift of sharp-leading-edged delta wings with blowing
The lift of sharp-leading-edged delta wings with blowing
By Domingo A. Tavella
Experimental studies of a delta wing with leading edge flaps
Experimental studies of a delta wing with leading edge flaps
By Chyang S. Lee
Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds
Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds
By Julio Chu
Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰
Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰
By M. Leroy Spearman
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
By Jim A. Penland