CHORDWISE LOADING AND CAMBER FOR TWO-DIMENSIONAL THIN SECTIONS
from $134.75
Effect of Chordwise Location of Maximum Thickness on the Supersonic Wave Drag of Sweptback Wings
from $110.00
DE-ICING AND RUNBACK CHARACTERISTICS OF THREE CYCLIC ELECTRIC, EXTERNAL DE-ICING BOOTS EMPLOYING CHORDWISE SHEDDING
from $129.70
Investigation of Effect of Span, Spanwise Location, and Chordwise Location of Spoilers on Lateral Control Characteristics of a Tapered Wing
DETERMINATION OF MEAN CAMBER SURFACES FOR WINGS HAVING UNIFORM CHORDWISE LOADING AND ARBITRARY SPANWISE LOADING IN SUBSONIC FLOW
HYDRODYNAMIC ASPECT OF PROPELLER DESIGN BASED ON LIFTING-SURFACE THEORY. PART II. ARBITRARY CHORDWISE LOAD DISTRIBUTION.
from $139.70
HYDRODYNAMIC ASPECT OF PROPELLER DESIGN BASED ON LIFTING-SURFACE THEORY. PART I. UNIFORM CHORDWISE LOAD DISTRIBUTION.
from $144.70
INVESTIGATION OF SPOILERS AT A MACH NUMBER OF 1.93 TO DETERMINE THE EFFECTS OF HEIGHT AND CHORDWISE LOCATION ON THE SECTION AERODYNAMIC CHARACTERISTICS OF A TWO-DIMENSIONAL WING
Section Characteristics of a 10.5-Percent-Thick Airfoil with Area Suction as Affected by Chordwise Distribution of Permeability
from $189.70
PREDICTION OF ROTOR INSTABILITY AT HIGH FORWARD SPEEDS. VOLUME I. STEADY FLIGHT DIFFERENTIAL EQUATIONS OF MOTION FOR A FLEXIBLE HELICOPTER BLADE WITH CHORDWISE MASS UNBALANCE.
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