Annual report of the National Advisory Committee for Aeronautics  1939

"Including Technical reports";United States Govrnment Printing Office 1934-1940年刊 の複製

「国立国会図書館デジタルコレクション」より

[目次]

  • TECHNICAL REPORTS
  • No.645. Correction of Temperatures of Air-Coolcd Engine Cylinders for Variation in Engine and Cooling Conditions.By Oscar W.Schey,Benjamin Pinkel,and Herman H.Ellerbrock,Jr.,N.A.C.A / 49
  • No.646. The Compressibility Burble and the Effect of Compressibility on Pressures and Forces Acting on an Airfoil.By John Stack,W.F.Lindsey,and Robert E.Littell,N.A.C.A / 73
  • No.647. Tests of N.A.C.A.0009,0012,and 0018 Airfoils in the Full-Scale Tunnel.By Harry J.Goett and W.Kenneth Bullivant,N.A.C.A / 97
  • No.648. Design Charts for Predicting Downwash Angles and Wake Characteristics Behind Plain and Flapped Wngs.By Abe Silverstein and S.Katzoff N.A.C.A / 107
  • No.649. The"Pack"Mcthod for Compressive Tests of Thin Specimens of Materials Used in Thin-Wall Structures.By C.S.Aitchison and L.B.Tuckerman,National Bureau of Standards / 133
  • No.650. The Aerodynamic Characteristics of Six Full-Scale Propellers Having Different Airfoil Sections.By David Biermann and Edwin P.Hartman,N.A.C.A / 145
  • No.651. Downwash and Wake Behind Plain and Flapped Airfoils.By Abe Silverstein,S.Katzoff,and W.Kenneth Bullivant,N.A.C.A / 179
  • No.652. Air Flow in the Boundary Layer of an Elliptic Cylinder.By G.B.Schubauer,National Bureau of Standards / 207
  • No.653. A Study of Air Flow in an Engine Cylinder.By Dana W.Lee,N.A.C.A / 227
  • No.654. General Airplane Performance.By W.C.Rockerfeller,California Institute of Technology / 241
  • No.655. The Knocking Characteristics of Fuels in Relation to Maximum Permissible Performance of Aircraft Engines.By A.M.Rothrock and Arnold E.Biermann,N.A.C.A / 267
  • No.656. The Column Strength of Two Extruded Aiuminum-Alloy H-Sections.By William R.Osgood and Marshall Holt,National Bureau of Standards and Aluminum Company of America / 289
  • No.657. The Influence of Directed Air Flow on Combustion in a Spark-Ignition Engine.By A.M.Rothrock and R.C.Spencer,N.A.C.A / 313
  • No.658. Tests of Two Full-Seale Propellers With Ditieront Pitch Distributions,at Blade Angles Up to 60°.By David Biermann and Edwin P.Hartman,N.A.C.A / 327
  • No.659. Effect of Service Stresses on Impact Resistance,X-Ray Diffraction Patterns,and Microstructure of 25S Aluminum Alloy.By J.A.Kies and G.W.Quick,National Bureau of Standards / 343
  • No.660. Experimental Investigation of the Momentum Method for Determining Profile Drag.By Harry J.Goett,N.A.C.A / 365
  • No.661. Tests in the Variable-Density Wind Tunnel of the N.A.C.A.23012 Airfoil With Plain and Split Flaps.By Ira H.Abbott and Harry Greenberg,N.A.C.A / 373
  • No.662. Design of N.A.C.A.Cowlings for Radial Air-Cooled Engines.By George W.Stickle,N.A.C.A / 383
  • No.663. The Effect of Continuous Weathering of Light Metal Alloys Used in Aircraft.By Willard Mutehler,National Bureau of Standards / 395
  • No.664. Wind-Tunnel Investigation of an N.A.C.A.23012 Airfoil With Various Arrangements-of Slotted Flaps.By Carl J.Wenzinger and Thomas A.Harris,N.A.C.A / 423
  • No.665. Calculation of the Aerodymanic Characteristics of Tapered Wings with Partial-Span Flaps.By Henry A.Pearson and Raymond F.Anderson,N.A.C.A / 455
  • No.666. Aircraft Rate-of-Climb Indicators.By Daniel P.Johnson,National Bureau of Standards / 473
  • No.667. Determination of the Profile Drag of an Airplane Wing in Flight at High Reynolds Numbers.By Joseph Bicknell,N.A.C.A / 483
  • No.668. Wind-Tunnel Investigation of N.A.C.A.23012,23021,and 23030 Airfoils With Various Sizes of Split Flap.By Carl J.Wenzinger and Thomas A.Harris,N.A.C.A / 493
  • No.669. Airfoil Section Data Obtained in the N.A.C.A.Variable-Density Tunnel as Affected by Support Interference and Other Corrections.By Eastman N.Jacobs and Ira H.Abbott,N.A.C.A / 507
  • No.670. Tensile Elastic Properties of 18:8 Chromum-Nickel Steel as Affected by Plastic Deformation.By D.J.McAdam,J.,and R.W.Mebs,National Bureau of Standards / 539
  • No.671. A Theoretical Study of the Moment on a Body in a Compressible Fluid.By Carl Kaplan,N.A.C.A / 581
  • No.672. Freen-Spinning Wind-Tunnel Tests of a Low-Wing Monoplane With Systematic Changes in Wings and Tails-IV.Effect of Center-of-Gravity Location.By Oscar Seidman and A.I.Neihouse,N.A.C.A / 599
  • No.673. Experimental Verification of the Theory of Oseillating Airfoils.By Abe Silverstein and Upshur T.Joyner,N.A.C.A / 619
  • No.674. Cooling on the Front of an Air-Cooled Engine Cylinder in a Conventional Engine Cowling.By M,J.Brevoort and U.T.Joyner,N.A.C.A / 625
  • No.675. Effects of Elevator Nose Shape,Gap,Balance,and Tabs,on the Aerodynamic Characteristics of a Horizontal Tail Surface.By Harry J.Goett and J.P.Reeder,N.A.C.A / 639
  • No.676. Surface Heat-Transfer Coefficients of Finned Cylinders.By Herman H.Ellerbrock,Jr.,and Arnold E.Biermann,N.A.C.A / 651
  • No.677. Wind-Tunnel Investigation of an N.A.C.A.23021 Airfoil With Various Arrangements of Slotted Flaps.By Carl J.Wenzinger and Thomas A.Harris,N.A.C.A / 665
  • No.678. Interference of Tail Surfaces and Wing and Fuselage From Tests of 17 Combinations in the N.A.C.A.Variable-Density Tunnel.By Albert Sherman,N.A.C.A / 689
  • No.679. Wind-Tunnel Investigation of an N.A.C.A.23012 Airfoil With a Slotted Flap and Three Thpes of Auxiliary Flap.By Carl J.Wenzinger and William E.Gauvain,N.A.C.A / 699
  • No.680. The Effect of Nacelle-Propeller Diameter Ratio on Body Interference and on Propeller and Cooling Characteristics.By James G.McHugh and Eldridge H.Derring,N.A.C.A / 727

「国立国会図書館デジタルコレクション」より

この本の情報

書名 Annual report of the National Advisory Committee for Aeronautics
著作者等 アメリカ合衆国航空諮問委員会
巻冊次 1939
出版元 Bunseisha
刊行年月 昭和19
ページ数 6冊
大きさ 27cm
全国書誌番号
22010863
※クリックで国立国会図書館サーチを表示
言語 英語
出版国 日本
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