2 edition of Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber found in the catalog.
Surface-pressure and flow-visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading-edge radius and camber
1996 by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, D.C, Springfield, Va .
Written in English
|Other titles||Surface pressure and flow visualization data at Mach number of 1.60 for three 65 ̊delta wings varying in leading edge radius and camber|
|Statement||S. Naomi McMillin ... [et al.].|
|Series||NASA technical memorandum -- 4673|
|Contributions||McMillin, S. Naomi, United States. National Aeronautics and Space Administration.|
|The Physical Object|
Acoustic Analysis of Hydrodynamic Oscillations in the Gentilly-1 Steam Mains.
Ivy takes care
kinetics of the reaction of sodium amalgam with aqueous solutions of acids at a liquid-liquid interface
Kung Fu Panda Fold Out
Roger Miller, or, Heroism in humble life
Moi and O.B. Shanks
Turfgrass Diseases and Insect Pests (Descriptions, Illustrations and Controls).
Manifest of passengers arriving in the St. Albans, VT District through Canadian Pacific, and Atlantic Ports, 1895-1954
Dead mans grip
United Scriptures examination, 1958.
Securing the four sides of the nation
The Kasîdah (couplets) of Hâjî Abdû el-Yezdî
HyperSource on optical technologies