Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing
Explore the source record for details and available documents.
Schneider, William C↗
Engineering topics
Schneider, William C
Publications and source records attributed to Schneider, William C.
Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers
Explore the source record for details and available documents.
Schneider, William C↗
Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303
Explore the source record for details and available documents.
Foster, Gerald V↗
Development of a New Flutter Testing Technique Using a Towed Dynamic Airplane Model Equipped with an Automatic Stabilizing System
Explore the source record for details and available documents.
Schneider, William C↗
Effects of Mach Number Variation Between 0.07 and 0.34 and Reynolds Number Variation Between 0.97 x 10(exp 6) and 8.10 x 10(exp 6) Power on the Maximum Lift Coefficient of a Wing of NACA 64-210 Airfoil Sections
Explore the source record for details and available documents.
SURFACE CONDITIONS - COMPLETE WINGS↗
A comparison of the spanwise loading calculated by various methods with experimental loadings obtained on a 45 degrees sweptback wing of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)
Explore the source record for details and available documents.
Schneider, William C↗