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31. NACA research memorandum RM (series). L58A23. Aerodynamic characteristics over Mach number range of 1.40 to 2.78 of rocket-propelled airplane configuration having low 52.5° delta wing and unswept horizontal tail [with list of references]: by Alan B. Kehlet. Washington, Mar. 6, 1958

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

32. NACA research memorandum RM (series). L58A27. Jet effects on base drag of cylindrical afterbody with extended nozzles [with list of references]: by William J. Nelson and William R. Scott. Washington, Apr. 15, 1958

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

33. NACA research memorandum RM (series). L58B14. Ground simulator studies of small side-located controller in power control system [with list of references]; by Arthur Assadourian. Washington, Apr. 23, 1958

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

34. NACA research memorandum RM (series). L58B26. Low-speed investigation of effects of frequency and amplitude of oscillation in sideslip on lateral stability derivatives of 60° delta wing, 45° sweptback wing, and unswept wing [with list of references]; by Jacob H. Lichtenstein and James L. Williams. Washington, June 5, 1958.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

35. NACA research memorandum RM (series). L58C11. Wind-tunnel investigation at Mach number of 2.01 of forebody strakes for improving directional stability of supersonic aircraft [with list of references]; by Cornelius Driver. Washington, May 26, 1958.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

36. NACA research memorandum RM (series). L58C13. Effects of external store-pylon configuration and position on aerodynamic characteristics of 45° swept wing-fuselage combination at Mach number of 1.61 [with list of references]; by Odell A. Morris. Washington, May 13, 1958.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

37. NACA research memorandum RM (series). L58C18. Effects of vertical location of wing and horizontal tail on static lateral and directional stability of trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01 [with list of references]; by Ross B. Robinson. Washington, July 9, 1958.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

38. NACA research memorandum RM (series). L58D09. Pressure loads produced on flat-plate wing by rocket jets exhausting in spanwise direction below wing and perpendicular to free-stream flow of Mach number 2.0 [with list of references]; by Ralph A. Falanga and Joseph J. Janos. Washington, June 5, 1958.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [January 1961]
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

39. NACA research memorandum RM (series). L56H28. Investigation of ejection release of several dynamically scaled bluff internal stores at Mach numbers 0.8, 1.39, and 1.98 (with list of references]; by Howard S. Carter and John B. Lee.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Dec. 26, 1960
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

40. NACA research memorandum RM (series). A56L05. Deductions in temperature-recovery factor associated with pulsating flows generated by spike-nosed cylinders at Mach numbers of 3.50 [with list of references]; by C. A. Hermach, Samuel Kraus, and John O. Reller, jr. Washington, Mar. 4, 1957

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: [December 1960]
SuDoc number:: Y 3.N 21/5:15/A 56 L 05

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