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additions airplane alloys analysis angle of attack angle of sideslip annealing assigned boattail boundary calculated characteristics chondrite classification Classification Map clusters coefficient comparison containing Continued data set deflection determined diffuser drag effects equations error Figure flap flow friction function geometry given increased indicate input lift loading loss Mach number maximum measure method NASA obtained output parameters percent performance points position presented pressure range ratio reference response Reynolds number samples shown shows similarity space spoiler surface TECHNICAL techniques temperature term test section tion toughness values vane variation wall wear wind tunnel wing
Page 1 - NASA Langley Research Center Hampton, Va. 23665 11. Contract or Grant No 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address...
Page 78 - SI and US Customary Units. The measurements and calculations were made in US Customary Units.
Page 39 - No. 12. Sponsoring Agency Name and Address National Aeronautics and Space Administration Washington, DC 20546 and US Army Air Mobility R&D Laboratory Moffett Field, CA 94035 13.
Page 13 - Gillis, Clarence L., Polhamus, Edward C., and Gray, Joseph L., Jr.: Charts for Determining Jet -Boundary Corrections for Complete Models in 7- by 10-Foot Closed Rectangular Wind Tunnels.
Page 15 - An Investigation of the Plastic Fracture of AISI 4340 and 18 Nickel-200 Grade Maraging Steels," Metallurgical Transactions A, Vol.
Page 1 - For sale by the National Technical Information Service. Springfield, Virginia 22161 1 Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA CR-2885 4. Title and Subtitle 5. Report Date "Computers for Real Time Market Survey" Flight Simulation: A July 1977 6.
Page 10 - Friction and Wear Characteristics of Polyimide and Filled Polyimide Compositions in Vacuum (10~] ° mm Hg).