Wing Profiles

29 books
Theory of wing sectionsIra H. Abbott
⏱ 11h 33m

Theory of wing sections

Ira H. Abbott

1959693 pp.
Recent developments in augmentor-wing aerofoil sectionsJ. D. Lye
⏱ 12m

Recent developments in augmentor-wing aerofoil sections

J. D. Lye

198712 pp.
Static aeroelastic analysis of a three-dimensional generic wingJohn A. Green
⏱ 26m

Static aeroelastic analysis of a three-dimensional generic wing

John A. Green

199026 pp.
Basic wing and airfoil theoryPope, Alan
⏱ 4h 54m

Basic wing and airfoil theory

Pope, Alan

1951294 pp.
Airfoil dynamic stall and rotorcraft maneuverabilityWilliam G. Bousman

Airfoil dynamic stall and rotorcraft maneuverability

William G. Bousman

2000No page data
In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)Edwin J. Saltzman

In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)

Edwin J. Saltzman

1994No page data
Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speedsUnknown Author

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds

Unknown Author

2001No page data
Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary CelebrationF-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.)

Proceedings of the F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration

F-8 Digital Fly-By-Wire and Supercritical Wing First Flight's 20th Anniversary Celebration (1992 Edwards, Calif.)

1996No page data
In-flight and simulated aircraft fuel temperature measurementsRoger A. Svehla

In-flight and simulated aircraft fuel temperature measurements

Roger A. Svehla

1990No page data
Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wingsKen Craig
⏱ 37m

Computational study of the aerodynamics and control by blowing of asymmetric vortical flows over Delta wings

Ken Craig

199137 pp.
TrandesnfJen-Fu Chang

Trandesnf

Jen-Fu Chang

1987No page data
Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselagesVenkit Iyer

Computation of three-dimensional compressible boundary-layers to fourth-order accuracy on wings and fuselages

Venkit Iyer

1990No page data
Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight dataRobert Alan Hess
⏱ 1h 3m

Effects of wing modification on an aircraft's aerodynamic parameters as determined from flight data

Robert Alan Hess

198663 pp.
Additional development of the XTRAN3S computer programChristopher J. Borland

Additional development of the XTRAN3S computer program

Christopher J. Borland

1989No page data
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊Scott P. Fears
⏱ 2h 25m

Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊

Scott P. Fears

1995145 pp.
Proceedings of the F-8 digital fly-by-wire and supercritical wing first flight's 20th anniversary celebrationUnknown Author

Proceedings of the F-8 digital fly-by-wire and supercritical wing first flight's 20th anniversary celebration

Unknown Author

1996No page data
Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillationsRobert M. Bennett

Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

Robert M. Bennett

1999No page data
Water tunnel flow visualization study through poststall of 12 novel planform shapesGregory M. Gatlin

Water tunnel flow visualization study through poststall of 12 novel planform shapes

Gregory M. Gatlin

1996No page data
Pressure distributions from subsonic tests of a NACA 0012 semispan wing modelZachary T. Applin

Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

Zachary T. Applin

1995No page data
Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoilDavid E. Hahne
⏱ 48m

Full-scale semispan tests of a business-jet wing with a natural laminar flow airfoil

David E. Hahne

199148 pp.
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