Airfoil Profiles

39 books
Computer program to obtain ordinates for NACA airfoilsUnknown Author

Computer program to obtain ordinates for NACA airfoils

Unknown Author

1996No page data
Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 106 to 9.0 x 106Laurence K. Loftin
⏱ 1h 15m

Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 106 to 9.0 x 106

Laurence K. Loftin

194975 pp.
Direct calculation of airfoils from pressure distributionRichard Eppler
⏱ 1h 1m

Direct calculation of airfoils from pressure distribution

Richard Eppler

197461 pp.
Recent developments in augmentor-wing aerofoil sectionsJ. D. Lye
⏱ 12m

Recent developments in augmentor-wing aerofoil sections

J. D. Lye

198712 pp.
A comparison of design variables for control theory based airfoil optimizationJames Reuther

A comparison of design variables for control theory based airfoil optimization

James Reuther

1995No page data
Airfoil dynamic stall and rotorcraft maneuverabilityWilliam G. Bousman

Airfoil dynamic stall and rotorcraft maneuverability

William G. Bousman

2000No page data
Control of unsteady separated flow associated with the dynamic stall of airfoilsMichael C. Wilder

Control of unsteady separated flow associated with the dynamic stall of airfoils

Michael C. Wilder

1992No 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
Study by double exposure holography of the three-dimensional character of the flow around an airfoil profile in a wind tunnelG. Heid

Study by double exposure holography of the three-dimensional character of the flow around an airfoil profile in a wind tunnel

G. Heid

1986No 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.
Improving CPA-TSD steady pressure solutions through airfoil slope modificationUnknown Author

Improving CPA-TSD steady pressure solutions through airfoil slope modification

Unknown Author

1996No page data
Improving CPA-TSD steady pressure solutions through airfoil slope modificationUnknown Author

Improving CPA-TSD steady pressure solutions through airfoil slope modification

Unknown Author

1996No page data
Improving CPA-TSD steady pressure solutions through airfoil slope modificationUnknown Author

Improving CPA-TSD steady pressure solutions through airfoil slope modification

Unknown Author

1996No page data
Improving CPA-TSD steady pressure solutions through airfoil slope modificationUnknown Author

Improving CPA-TSD steady pressure solutions through airfoil slope modification

Unknown Author

1996No page data
Control theory based airfoil design for potential flow and a finite volume discretizationJames Reuther

Control theory based airfoil design for potential flow and a finite volume discretization

James Reuther

1995No page data
TrandesnfJen-Fu Chang

Trandesnf

Jen-Fu Chang

1987No page data
Determination of the pressure drag of airfoils by integration of surface pressuresWilliam H. Phillips

Determination of the pressure drag of airfoils by integration of surface pressures

William H. Phillips

1990No page data
Effect of acoustic excitation on stalled flows over an airfoilK. B. M. O. Zaman

Effect of acoustic excitation on stalled flows over an airfoil

K. B. M. O. Zaman

1990No page data
A feasibility study to control airfoil shape using THUNDERJennifer L. Pinkerton

A feasibility study to control airfoil shape using THUNDER

Jennifer L. Pinkerton

1997No page data
PROFILELeslie Collins

PROFILE

Leslie Collins

1997No page data
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