TY - GEN

AU - United States Congress House

AU - United States President (1933-1945 : Roosevelt)

AU - United States National Advisory Committee for Aeronautics

AU - Becker, John V.

AU - Bell, E. Barton

AU - Biermann, David

AU - Chiarito, Patrick T.

AU - Cohen, Doris

AU - Conway, Robert N.

AU - Delano, James B.

AU - Diehl, Walter S.

AU - Garrick, I.E

AU - Harris, Thomas A.

AU - Hartman, Edwin P.

AU - Jones, Robert Thomas

AU - Kaplan, Carl

AU - Katzoff, S.

AU - Kuhn, Paul

AU - Leonard, Lloyd H.

AU - Levy, Samuel

AU - Lowry, John G.

AU - Lundquist, Eugene E.

AU - Silverstein, Abe

AU - McPherson, Albert E.

AU - Spano, Bartholomew S.

AU - Miller, Cearcy D.

AU - Stowell, Elbridge Z.

AU - Rogallo, Francis M.

AU - Roosevelt, Franklin Delano

AU - Sweberg, Harold H.

AU - Wilson, Herbert A.

AU - Recant, Isidore G.

AU - Robinson, Russell Gideon

AU - Theodorsen, Theodore

AU - Ramberg, Walter

TI - Twenty-eighth annual report of the National Advisory Committee for Aeronautics, 1942. Including technical reports Nos. 727 to 751

PY - 1943

N2 - A study by high-speed photography of combustion and knock in a spark-ignition engine, by Cearcy D. Miller [No. 727], p. 15

N2 - An investigation of the drag of windshields in 8-foot high-speed wind-tunnel, by Russell G. Robinson and James B. Delano [No. 730], p. 65

N2 - Bending of rectangular plates with large deflections, by Samuel Levy [No. 737], p. 139

N2 - Critical compressive stress for flat rectangular plates supported along all edges and elastically restrained against rotation along the unloaded edges, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 733], p. 99

N2 - Critical compressive stress for outstanding flanges, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 734], p. 111

N2 - Determination of optimum plan forms for control surfaces, by Robert T. Jones and Doris Cohen [No. 731], p. 79

N2 - Drag and propulsive characteristics of air-cooled engine-nacelle installations for large airplanes, by Abe Silverstein and Herbert A. Wilson, Jr. [No. 746], p. 301

N2 - Flutter calculations in three degrees of freedom, by Theodore Theodorsen and I.E. Garrick [No. 741], p. 223

N2 - Ground effect on downwash angles and wake location, by S. Katzoff and Harold H. Sweberg [No. 738], p. 159

N2 - High-speed tests of a model twin-engine low-wing transport airplane, by John V. Becker and Lloyd H. Leonard [No. 750], p. 391

N2 - High-speed tests of conventional radial-engine cowlings, by Russell G. Robinson and John V. Becker [No. 745], p. 287

N2 - Investigation in the 7-by 10-foot wind-tunnel of ducts for cooling radiators within an airplane wing, by Thomas A. Harris and Isidore G. Recant [No. 743], p. 249

N2 - List of technical reports, p. III

N2 - Non-stationary flow about a wing-aileron tab combination including aerodynamic balance, by Theodore Theodorsen and I.E. Garrick [No. 736], p. 129

N2 - Normal pressure tests of circular plates with clamped edges, by Albert E. McPherson, Walter Ramberg, and Samuel Levy [No. 744], p. 269

N2 - Normal-pressure tests of rectangular plates, by Walter Ramberg, Albert E. McPherson, and Samuel Levy [No. 748], p. 349

N2 - On the use of residue theory for treating the subsonic flow of a compressible fluid, by Carl Kaplan [No. 728], p. 39

N2 - Pressure distribution over an NACA 23012 airfoil with a fixed slot and a slotted flap, by Thomas A. Harris and John G. Lowry [No. 732], p. 85

N2 - Propeller charts for the determination of the rotational speed for the maximum ration of the propulsive efficiency to the specific fuel consumption, by David Biermann and Robert N. Conway [No. 749], p. 373

N2 - Restraint provided a flat rectangular plate by a study stiffener along an edge of the plate, by Eugene E. Lundquist and Elbridge Z. Stowell [No. 735], p. 123

N2 - Shear lag in box beams: Methods of analysis and experimental investigations, by Paul Kuhn and Patrick T. Chiarito [No. 739], p. 171

N2 - Square plate with clamped edges under normal pressure producing large deflections, by Samuel Levy [No. 740], p. 209

N2 - Test of a single-stage axial flow-fan, by E. Barton Bell [No. 729], p. 49

N2 - The mean aerodynamic chord and the aerodynamic center of a tapered wing, by Walter S. Diehl [No. 751], p. 413

N2 - Wind-tunnel investigation of an NACA 23012 airfoil with 30-percent-chord venetian-blind flaps, by F.M. Rogallo and Bartholomew S. Spano [No. 742], p. 241

N2 - Wind-tunnel tests of four- and six-blade single- and dual-rotating tractor propellers, by David Biermann and Edwin P. Hartman [No. 747], p. 319

BT - United States congressional serial set ; serial set no. 10825

BT - House document / 78th Congress, 1st session. House ; no. 146

CY - Washington, DC

UR - http://slubdd.de/katalog?TN_libero_mab2

ER -