Format:
Online-Ressource (433 p)
,
illustrations, tables
Edition:
Online-Ausg. Chester, Vt NewsBank, inc 2008 U.S. Congressional Serial Set, 1817-1980
Series Statement:
United States congressional serial set serial set no. 10678
Note:
A graphical method of determining pressure distribution in two-dimensional flow, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 722], p. 313
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A high-speed motion-picture study of normal combustion, knock, and preignition in a spark-ignition engine, by A.M. Rothrock, R.C. Spencer, and Cearcy D. Miller, N.A.C.A. [No. 704], p. 15
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A simplified theoretical method of determining the characteristics of a lifting rotor in forward flight, by F.J. Bailey, Jr., N.A.C.A. [No. 716], p. 209
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An analysis of the stability of an airplane with free controls, by Robert T. Jones and Doris Cohen, N.A.C.A. [No. 709], p. 109
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An apparatus for measuring rates of discharge of a fuel-injection system, by Francis J. Dutee, N.A.C.A. [No. 714], p. 193
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Analysis and prediction of longitudinal stability of airplanes, by R.R. Gilruth and M.D. White, N.A.C.A. [No. 711], p. 137
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Appendix, p. 118
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Determination of control-surface characteristics from NACA plain-flap and tab data, by Milton B. Ames, Jr. and Richards I. Sears, N.A.C.A. [No. 721], p. 295
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Effect of aging on mechanical properties of aluminum-alloy rivets, by Frederick C. Roop, National Bureau of Standards [No. 724], p. 353
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Effect of body nose shape on the propulsive efficiency of a propeller, by G.W. Stickle, John L. Crigler, and Irven Naiman, N.A.C.A. [No. 725], p. 371
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Flow coefficients of monosleeve valves, by C.D. Waldron, N.A.C.A. [No. 717], p. 227
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Internal-flow systems for aircraft, by F.M. Rogallo, N.A.C.A. [No. 713], p. 165
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Lateral control required for satisfactory flying qualities based on flight tests of numerous airplanes, by R.R. Gilruth and W.N. Turner, N.A.C.A. [No. 715], p. 201
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Preignition characteristics of several fuels under simulated engine conditions, by R.C. Spencer, N.A.C.A. [No. 710], p. 121
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Pressure available for cooling with cowling flaps and tab data, by George W. Stickle, Irven Naiman, and John L. Crigler, N.A.C.A. [No. 720], p. 283
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Pressure distribution over an NACA 23021 airfoil with a slotted and a split flap, by Thomas A. Harris and John G. Lowry, N.A.C.A. [No. 718], p. 241
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Propeller analysis from experimental data, by George M. Stickle and John L. Crigler, N.A.C.A. [No. 712], p. 147
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Tests of the NACA 0025 and 0035 airfoils in the full-scale wind tunnel, by W. Kenneth Bullivant, N.A.C.A. [No. 708], p. 91
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The additional-mass effect of plates as determined by experiments, by William Gracey, N.A.C.A. [No. 707], p. 81
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The design of fins for air-cooled cylinders, by Arnold E. Biermann and Herman H. Ellerbrock, Jr. [No. 726], p. 401
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The problem of cooling an air-cooled cylinder on an aircraft engine, by M.J. Brevoort and U.T. Joyner, N.A.C.A. [No. 719], p. 267
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Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double-slotted flaps, by Thomas A. Harris and Isidore G. Recant, N.A.C.A. [No. 723], p. 321
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Wind-tunnel investigation of effect of interference on lateral-stability characteristics of four NACA 23012 wings, an elliptical and a circular fuselage, and vertical fins, by Rufus O. House and Arthur R. Wallace, N.A.C.A. [No. 705], p. 31
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Wind-tunnel investigation of spoiler deflector, and slot lateral-control devices on wings with full-span split and slotted flaps, by Carl J. Wenzinger and Francis M. Rogallo, N.A.C.A. [No. 706], p. 51
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