Author: National Aeronautics and Space Administration / Sudoc Stem: Y 3.N 21/5 - Blacklight Search Results

Start Over Author National Aeronautics and Space Administration Sudoc Stem Y 3.N 21/5

1291. NACA research memorandum RM (series). E51G23. Force and pressure characteristics for series of nose inlets at Mach numbers from 1.59 to 1.99:5. Analysis and comparison on basis of ram-jet aircraft range and operational characteristics [with list of references]; by E. Howard, R. W. Luidens, and J. L. Allen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 13, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1292. NACA research memorandum RM (series). E51C15. Altitude-wind-tunnel investigation of performance characteristics of J47D protoype (RX1-1) turbojet endue with variable-area exhaust nozzle [with list of references]; by E. William Conrad and John E. McAulay.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 5, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1293. NACA research memorandums RM (series). E51E01. Performance characteristics of aircraft cooling ejectors having short cylindrical shrouds [with list of references]; by Fred D. Kochendorfer and Morris D. Rousso.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 22, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1294. NACA research memorandum RM (series). A51C08. Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of canard missile configuration [with list of references]; by J. Richard Spabr and Robert A. Robinson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: May 11, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1295. NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. L50G07. Langley 9-inch supersonic tunnel tests of several modifications of supersonic missile having tandem cruciform lifting surfaces: Three-component data results of models having ratios of wing span to tall span equal to and less than 1 and some static rolling-moment data [with one reference]; by Robert W. Rainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 7, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1296. NACA research memorandum RM (series). (National Advisory Committee for Aeronautics.) [Processed. No longer confidential.]. L50I29a. Langley 9-inch supersonic tunnel test of several modifications of supersonic missile having tandem cruciform lifting surfaces: Three-component data results of models having ratios of wing span to tail span less than 1 [with list of references]; by Robert W. Rainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Mar. 7, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1297. NACA research memorandum RM (series). L9L30. Langley 9-inch supersonic tunnel tests of several modifications of supersonic missile having tandem cruciform lifting surfaces, 3-component data results of models having ratios of wing span to tail span equal to 1; by Robert W. Rainey.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 7, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1298. NACA research memorandum RM (series). E50L04. Investigation at zero angle of attack of 16-inch ram-jet engine in 8-by 6-foot supersonic wind tunnel [with list of references]; by T. Nussdorfer, F. Wilcox and E. Perchonok.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 2, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1299. NACA research memorandum RM (series). L50K17. Preliminary investigation of fin-actuated jet-vane control system for stabilization of rocket-powered models [with list of references]; by Andrew R. Wineman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 17, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

1300. NACA research memorandum RM (series). A50H10. Lateral-control characteristics and dihedral effect of wing-body combination with variable-incidence triangular wing and wing-tip ailerons at Mach number of 1.52 [with list of references]; by Richard Scherrer and David H. Dennis.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Jan. 10, 1951
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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