Annual report of the National Advisory Committee for Aeronautics  1933

"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.441. A Flight Investigation of the Spinning of the NY-1 Airplane with Varied Mass Distribution and other Modifications,and an Analysis Based on Wind-Tunnel Tests.By Nathan F.Schudder / 37
  • No.442. A comparison Between the Theoretical and Measured Longitudinal Stability Characteristics of an Airplane.By Hartley A.Soule and John B.Wheatley / 53
  • No.443. Pressure-Distribution Measurements on the Hull and Fins of a1/40-Scale Model of the U.S.Airship Airship Akron.By Hugh B.Freeman / 67
  • No.444. Wind-Tunnel Research Comparing Lateral Control Devices Partieularly at High Angles of Attack.VI-Skewed Ailerons on Rectangular Wings.By Fred E.Weick and Thomas A.Harris / 81
  • No.445. Working Charts for the Determination of the Lift Distribution Between Biplane Wings.By Paul Kuhn / 93
  • No.446. Airfoil Section Characteristics as Affected by Protuberances.By Eastman N.Jacobs / 109
  • No.447. Static Thrust of Airplane Propellers.By Walter S.Diehl / 125
  • No.448. Improved Apparatus for the Measurement of Fluotuations of Air Speed in Turbulent Flow.By W.C.Mock,Jr.,and H.L.Dryden / 131
  • No.449. Wing Characteristics as Affected by Protuberances of Short Span.By Eastman N.Jacobs and Albert Sherman / 155
  • No.450. The Calculation of Take-Off Run.By Walter S.Diehl / 163
  • No.451. The Drag of Two Streamline Bodies as Affected by Protuberances and Appendages.By Ira H.Abbott / 171
  • No.452. General Potential Theory of Arbitrary Wing Sections.By T.Theodorsen and I.E.Garrick / 177
  • No.453. The Estimation of Maximum Load Capacity of Seaplanes and Flying Boats.By Walter S.Diehl / 211
  • No.454. Photomicrographic Studies of Fuel Sprays.By Dana W.Lee and Robert C.Spencer / 215
  • No.455. Penetration and Duration of Fuel Sprays from a Pump Injection System.By A.M.Rothrock and E.T.Marsh / 241
  • No.456. The Aerodynamic Forces and Moments Exerted on A Spinning Model of the NY-1 Airplane as Measured by the Spinning Balance.By M.J.Bamber and C.H.Zimmerman / 249
  • No.457. Maneuverability Investigation of an O3U-1 Observation Airplane.By F.L.Thompson and H.W.Kirschbaum / 263
  • No.458. Relative Loading on Biplane Wings.By Walter S.Diehl / 275
  • No.459. The N.A.C.A.Full-Scale Wind Tunnel.By Smith J.De France / 291
  • No.460. The Characteristics of 78 Related Airfoil Sections from Tests in the Variable-Density Wind Tunnel.By Eastman N.Jacobs,Kenneth E.Ward,and Robert M.Pinkerton / 299
  • No.461. Interference on an Airfoil of Finite Span in an Open Rectangular Wind Tunnel.By Theodore Theodorsen / 355
  • No.462. Tests of Nacelle-Propeller Combinations in Various Positions with Reference to Wings.III-Clark Y Wing-Various Radial-Engine Cowlings-Tractor Propeller.By Donald H.Wood / 359
  • No.463. The N.A.C.A.High-Speed Wind Tunnel and Tests of Six Propeller Sections.By John Stack / 399
  • No.464. Negative Thrust and Torque Characteristics of an Adjustable-Pitch Metal Propeller.By Edwin P.Hartmen / 421
  • No.465. Determination of the Theoretical Pressure Distribution for Twenty Airfoils.By I.E.Garrick / 433
  • No.466. Aircraft Power-Plant Instruments.By Harcourt Sontag and W.G.Brombacher / 447
  • No.467. The Experimental Determination of the Moments of Inertia of Airplanes.By Hartley A.Soule and Marvel P.Miller / 501
  • No.468. The Interference Between Struts in Various Combinations.By David Biermann and William H.Herrnstein,Jr / 515
  • No.469. Increasing the Air Charge and Scavenging the Clearance Volume of a Compression-Ignition Engine.By J.S.Spanogle,C.W.Hicks,and H.H.Foster / 525
  • No.470. The N.A.C.A.Tank-A High-Speed Towing Basin for Testing Models of Seaplane Eloats.By Starr Truscott / 535
  • No.471. Performance of a Fuel-Injection Spark-Ignition Engine Using a Hydrogenated Safety Fuel.By Oscar W.Schey and Alfred W.Young / 557
  • No.472. Wind-Tunnel Tests on Combinations of a Wing With Fixed Auxiliary Airfoils Having Various Chords and Profiles By Fred E.Weick and Robert Sanders / 567
  • No.473. Strength Tests of Thin-Walled Duralumin Cylinders in Compression.By Eugene E.Lundquist / 585
  • No.474. Nomenclature for Aeronautics.By National Advisory Committee for Aeronautics / 603

「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 1933
出版元 Bunseisha
刊行年月 昭和18
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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