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17331. 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.)

17332. 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.)

17333. 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.)

17334. 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.)

17335. NACA research memorandum RM (series). A51J10. Investigation of control-surface flutter derivatives of NACA 651-213 airfoil in Ames 16-foot high-speed wind tunnel [with list of references]; by John A. Wyss and Robert M. Sorenson.

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

17336. NACA research memorandum RM (series). E50F28. Altitude performance characteristics of turbojet-engine tail-pipe burner with variable-area exhaust nozzle using several fuel systems and flame holders [with list of references]; by LaVern A. Johnson and Carl L. Meyer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 29, 1950
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17337. NACA research memorandum RM (series). E50G13. Altitude performance characteristics of tall-pipe burner with converging conical burner section on J47 turbojet engine [with list of references]; by William R. Prince and John B. McAulay.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 19, 1950
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17338. NACA research memorandum RM (series). L50I20. Experimental investigation of flat-plate paddle jet vane operating on rocket jet [with list of references]; by Aleck C. Bond.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 15, 1950
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17339. NACA research memorandum RM (series). L50I06a. Determination of longitudinal stability of Bell X-1 airplane from transient responses at Mach numbers up to 1.12 at lift coefficients of 0.3 and 0.6 [with list of references]; by Ellwyn E. Angle and Euclid C. Holleman.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Nov. 7, 1950
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17340. NACA research memorandum RM (series). L50H29a. Preliminary results of flight investigation between Mach numbers of 0.80 and 1.36 of rocket-powered model of supersonic airplane configuration having tapered wing with circular-arc sections and 40° sweepback [with list of references]; by Charles T. D'Aiutolo and Homer P. Mason.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 31, 1950
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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