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NACA TN 116 Comparative Performance With Direct and Geared Engines
NACA TN 116 Comparative Performance With Direct and Geared Engines
Tunnel Wall Interference in V/STOL and High Lift Testing · Wall. NACA TN-l244,M,8 pp. No-dimensional span-loading tests were made of a two-foot-chord NACA 65,-012 airfoil model in
Tunnel Wall Interference in V/STOL and High Lift Testing · Wall. NACA TN-l244,M,8 pp. No-dimensional span-loading tests were made of a two-foot-chord NACA 65,-012 airfoil model in
NACA TN 1973 - Theoretical Spanwise Lift Distributions for Low Aspect Ratio Wings
NACA TN 1973 - Theoretical Spanwise Lift Distributions for Low Aspect Ratio Wings
NACA TN 4237
NACA TN 4237
NACA TN 942 Shear Strength of Rivets Affected by D t Ratios
NACA TN 942 Shear Strength of Rivets Affected by D t Ratios
naca.central.cranfield.ac.uknaca.central.cranfield.ac.uk/reports/1938/naca-tn-663.pdf · Created Date: Wed Nov 10 04:08:01 1999
naca.central.cranfield.ac.uknaca.central.cranfield.ac.uk/reports/1938/naca-tn-663.pdf · Created Date: Wed Nov 10 04:08:01 1999
NACA TN 102 Skin frictional resistance of plane surfaces in air
NACA TN 102 Skin frictional resistance of plane surfaces in air
NACA TN 2229 - The Effect of End Plates on Swept Wings at Low Speed
NACA TN 2229 - The Effect of End Plates on Swept Wings at Low Speed