Aerodynamical balance for P-1B and P-5 airplanes by standard analytical method for determination of center of gravity and mean average chord (reference to Curtiss Airplane and Motor Company's report numbers 3018 of Apr. 29, 1927) (Airplane Branch report).

Determination of structural airplane drag (Airplane Branch report).
Published: (1928)

Study of pressure distribution data (Airplane Branch report).
Published: (1927)

Wind tunnel test of 1/20 scale model of Materiel Division night observation airplane (Airplane Branch report).
Published: (1928)

Wind-tunnel test of PW-4 airplane (Airplane Section report).
Published: (1924)

Methods of correcting longitudinal balance of JN-6H airplanes.
Published: (1920)

Wind tunnel test of A-1 (ambulance) airplane (Airplane Section report).
Published: (1924)

Effect of sweep back and sweep forward on airfoil (Airplane Section report).
Published: (1926)

Induced drag of any biplane (Airplane Branch report).
Published: (1927)

Wind tunnel test of Thomas-Morse MP-3 airplane (Airplane Section report).
Published: (1924)

Wind tunnel test of DB-1 revised airplane model (Airplane Section report).
Published: (1924)

Aerodynamics of the airplane /
by: Millikan, Clark Blanchard, 1903-1966
Published: (1941)

Airplane aerodynamics /
by: Dommasch, Daniel O. (Daniel Otto), 1921-
Published: (1951)

Airplane aerodynamics /
by: Dommasch, Daniel O. (Daniel Otto), 1921-
Published: (1957)

Wind tunnel test of 36x6 airfoils (Airplane Section report).
Published: (1924)

Wind tunnel test of Junker L-6 monoplane (Airplane Branch report).
Published: (1922)

Wind tunnel test of 1/24 scale model of Douglas O-2E-1 airplane wing cellule through 360 degrees (Airplane Branch report).
Published: (1928)

Wind tunnel test of GA-2A ground attack airplane (Airplane Section report).
Published: (1924)

Report on wind-tunnel test of armored pursuit airplane PG-1, type IV.
Published: (1921)

Report of wind tunnel test on Gottingen No. 227 aerofoil (Airplane Section, S. and A. Branch).
Published: (1921)

Effect of cellule arrangement on rate of autorotation calculated by "strip" method (Airplane Branch report).
Published: (1928)

Report on wind tunnel test of Messenger airplane.
Published: (1920)

Wind tunnel test aileron characteristics as affected by design and by airfoil thickness (Airplane Section report).
Published: (1925)

Wing flap test of DH-4B wind tunnel model (Airplane Section report).
Published: (1926)

Report of wind tunnel test of corps observation CO-1 model (Airplane Section, S. and A. Branch).
Published: (1922)

Report on wind tunnel test of U.S.A.-27-C modified airfoil (Airplane Section, S. and A. Branch).
Published: (1922)

Wind tunnel tests of DH-4B model fitted with various fins and rudders (Airplane Branch report).
Published: (1927)

Simple aerodynamics and the airplane /
by: Carter, Clifton Carroll, 1876-1950
Published: (1940)

Simple aerodynamics and the airplane /
by: Monteith, Charles Norton, 1893-1940
Published: (1929)

Notes on airplane performance from standpoint of modern conception of drag (Airplane Section report).
Published: (1926)

Wind tunnel test of Fokker PW-5 with V-40 wing and PW-5 wing (Airplane Section report).
Published: (1924)

Report on wind tunnel test of Laddon night pursuit airplane.
Published: (1920)

Report of wind tunnel test on U.S.A. airfoils 30, 31, 32, 33, and 34 (Airplane Section, S. and A. Branch).
Published: (1921)

Report of wind tunnel test on R.A.F. 19, Springer No. 3, and Gottingen No. 244 (Airplane Section, S. and A. Branch).
Published: (1921)

Wind tunnel test of 6 horizontal tail surface designs having U.S.A.-47 airfoil section (Airplane Section report).
Published: (1925)

Airplane aerodynamics and performance /
by: Roskam, Jan, 1930-
Published: (1997)

Visual study of flow discontinuity on 6x13 .15 cylindrical camber airfoil (report of 14 Wind Tunnel Test No. 610) (Airplane Section report).
Published: (1926)