Author: National Aeronautics and Space Administration / Publisher: National Aeronautics and Space Administration - Blacklight Search Results

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17111. NACA research memorandum RM (series). E54G15. Pumping characteristics for several simulated variable-geometry ejectors [with list of references]; by John L. Allen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 8, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17112. NACA research memorandum RM (series). E54E11. Performance of pair of tubular combustors with external pilot chamber [with list of references]; by Robert Friedman and Eugene V. Zettle.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 7, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17113. NACA research memorandum RM (series). E54F24a. Effect of design over-all compressor pressure ratio division on 2-spool turbojet-engine performance and geometry [with list of references]; by James F. Dugan, jr..

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 7, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17114. NACA research memorandum RM (series). E54G12. Altitude investigation of 20-inch-diameter ram-jet engine with annularpiloted combustor [with list of references]; by James G. Henzel jr., and Arthur M. Trout.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 27, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17115. NACA research memorandum RM (series). E54F07. Performance characteristics of several full-scale double-shroud ejector configurations over range of primary gas temperatures [with list of references]; by William K. Greathouse.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Aug. 19, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17116. NACA research memorandum RM (series). E54F0S. Characteristics of flow about axially symmetric isentropic spikes for nose inlets at Mach number 3.85 [with list of references]; by James F. Connors and Richard R. Woollett.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 19, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17117. NACA research memorandum RM (series). E54E13. Effect of unequal air-flow distribution from twin inlet ducts on performance of axial-flow turbojet engine; by Curtis L. Walker, Joseph N. Sivo, and Emmert T. Jansen

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 3, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17118. NACA research memorandum RM (series). E54F17. Investigation of high-temperature single-stage turbine suitable for air cooling and turbine stator adjustment: 2, Performance of VorteX turbine at various stator settings [with list of references]: by Thomas R. Heaton, Donald E. Holeski, and Robert E. Forrette.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 3, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17119. NACA research memorandum RM (series). E54E20. Effect of wedge-type boundary-layer diverters on performance of halfconical side inlets at Mach number 2.96 [with list of references]; by Harry W. Johnson and Thomas G. Piercy.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 2, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

17120. NACA research memorandum RM (series). E54F04. Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics: 3, Effect of turbine stator adjustment [with list of references]: by Harold E. Rohlik and John J. Reheske.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Aug. 2, 1954
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

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