Aeronautical Engine^Ffti Aer Ering Aeronautical Engineerin Kjineering
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N O T I C E This Document Has Been Reproduced From
N O T I C E THIS DOCUMENT HAS BEEN REPRODUCED FROM MICROFICHE. ALTHOUGH IT IS RECOGNIZED THAT CERTAIN PORTIONS ARE ILLEGIBLE, IT IS BEING RELEASED IN THE INTEREST OF MAKING AVAILABLE AS MUCH INFORMATION AS POSSIBLE I 4 NASA Technical Memorandum 82788 NASA Research Activities in Aeropropuision N82-1bQE4 (Na,A-TM- m ,!7db ) NASA HESkAHCH A ,-T1V1T1kJ IN AEKOPRUNUL:iION j4ASA) 30 p HC A03 /Mr A01 CSCL 11L UUC138 G3/07 U88U5 John F. McCarthy, Jr. and Richard J. Weber Lewis Research Center Cleveland, Ohio ok- Prepared for the Twenty-fourth Israel Annual Conference on Aviation 8n(,' Astronautics Tel Aviv, Israel, February 17-18, 1982 t 4 ^6 1r X031 w tic.tiN, od` RV%SA ^ NASA RESEARCH AL'TIVITIES IN AEROPROPOLSION John F. McCarthy, Jr.* and Richard J. Weber National Aeronautics and Space Administration Lewis Research Center Cleveland, Ohio U.S.A. Abstract located in Cleveland,,Ohio, on the shore of We Erie, is responsible for aeropropulsion (as well NASA is a civilian agency of the U.S. govern- as related ground and space power). As shown in ment, responsible for advancing technologies re- the aerial photograph of Fig. 3, this is a very lated to air transportation. This paper describes substantial installation. The replacement value a sampling of the work at NASA's Lewis Research of our facilities is over 1-1/2 billion dollars; Center aimed at improved aircraft propulsion sys- our staff of 2700 engineers, scientists, and sup- W tems. Particularly stressed are efforts related port personnel has an annual research budget for to reduced noise and fuel consumption of subsonic aeropropulsion of about 125 million dollars. -
Aeronautical Engineering Case File Copy
NASA SP-7037 (80) AERONAUTICAL ENGINEERING CASE FILE COPY A SPECIAL BIBLIOGRAPHY WITH INDEXES Supplement 80 FEBRUARY 1977 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION ACCESSION NUMBER RANGES Accession numbers cited in this Supplement fall within the following ranges: STAR(N-10000 Series) N77-10001—N77-11966 IAA (A-10000 Series) A77-10001 -A77-12945 This bibliography was prepared by the NASA Scientific and Technical Information Facility operated for the National Aeronautics and Space Administration by Informatics Information Systems Company. NASA SP-7037(80) AERONAUTICAL ENGINEERING A Special Bibliography Supplement 80 A selection of annotated references to unclas- sified reports and journal articles that were introduced into the NASA scientific and tech- nical information system and announced in January 1 977 in • Scientific and Technical Aerospace Reports (STAR) • International Aerospace Abstracts (IAA) Scientific and Technical Information Office FEBRUARY 1977 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Washington, D.C. This Supplement is available from the National Technical Information Service (NTIS). Springfield, Virginia 22161, at the price code E02 ($475 domestic. $9 50 foreign) INTRODUCTION Under the terms of an interagency agreement with the Federal Aviation Administration this publication has been prepared by the National Aeronautics and Space Administration for the joint use of both agencies and the scientific and technical community concerned with the field of aeronautical engineering. The first issue of this bibliography -
2020-03-23T16:19:00+00:00Z PREVIOUS BIBLIOGRAPHIES in THIS SERIES NASA SF-Ls37 (07)
https://ntrs.nasa.gov/search.jsp?R=19710023698 2020-03-23T16:19:00+00:00Z PREVIOUS BIBLIOGRAPHIES IN THIS SERIES NASA SF-ls37 (07) AERONAUTICAL ENGINEERING A Special Bibliography Supplement 7 A selection of annotated references to unclas- sified reports and journal articles that were introduced into the NASA scientific and tech- nical information system and announced in .June 197 1 in Scientific and Technical Aerospace Reports (STAR) international Aerospace Abstracts IIAAI. Srieirrific aird Terhiriral Irrjoritroliorr OJJire OFFICE OF INDUSTRY AFFAIRS AND TECHNOLOGY UTILIZATION 197 I NATIONAL AERONAUTICS AND SPACE ADMINISTRATION INTRODUCTION Under the terms of an interagency agreement with the Federal Aviation Admin- istration this publication has been prepared by the National Aeronautics and Space Administration for the joint use of both agencies and the scientific and technical community concerned with the field of aeronautical engineering. This supplement to Aeroriaufical &iigirieeririg-A Special Bibliography (NASA SP-7037) Ii,[\ ~OOi-cpt)rl\. p~tiriial;ir~icIc\. ;ii,cl oihL,r Ll(,ciiiiicI (4 oi-i;iii;ill! ;i~ii~o~i~~cc~lIII .Iiriic 197 1 in Scietifific arid Technical Aerospace Reports (STAR/ or in liiferiiafiorial Aerospace Ahsfracfs (IAA). For previous bibliographies in this series, see inside of front cover. The coverage includes documents on the engineering and theoretical aspects of design, construction, evaluation, testing, operation, and performance of aircraft (includ- ing aircraft engines) and associated components, equipment, and systems. It also in- cludes research and development in aerodynamics, aeronautics, and ground support equipment for aeronautical vehicles. Each entry in the bibliography consists of a standard bibliographic citation accom- panied by an abstract. -
MA74-ZAB RAMJET Prime Contractor: the Marquardt Corporation Remarks Developed for Army Use, the MA 74-ZAB Is a Na- Celle-Type Su
MA74-ZAB RAMJET MA150-XAA RAMJET Prime Contractor: The Marquardt Corporation Prime Contractor: The Marquardt Corporation Remarks Remarks Developed for Army use, the MA 74-ZAB is a na The MA150-XAA is a nacelle-type subsonic and celle-type subsonic and supersonic ramjet engine supersonic ramjet engine with normal shock inle~. with normal shock inlet. It is the cruise propulsion It provides the cruise propulsion for the Army s source for the North American Redhead/Roadrunner North American Advanced Redhead/ Roadrunner tar target missile system for low altitude application. get missile system for high an?· low altitude applica tion. Specifications Specifications Length 90.7 inches; diameter 16.5 inches; weight 110 pounds; fuel JP-4; convergent sonic exit. Length 104.5 inches; diameter 19.0 inches; weight 165 pounds; fuel JP-4; convergent sonic exit. Performance Thrust 1,790 pounds net jet. Performance Thrust 2,300 pounds net jet at low altitude; 575 pounds net jet at high altitude. 480 ---- -- ------ ENGINES (TURBINE) T53 TURBOSHAFT GAS TURBINE E NGINE Prime Contractor: Lycoming Division, Avco Corpor ation Remarks T53 TURBOPROP GAS TURBINE E NGINE With over 1,500,000 hours of flight experience under Prime Contractor: Lycoming Division, Avco Corpor all environmental conditions, accumulating more ation than 11 ,000 hours monthly in Vietnam alone, the T53 turboshaft e ngine is the most experienced in its Remarks class in the world. Configurations of this engine powe r the Army's versatile Bell UH-1 " Huey" The latest version of the turboprop T53, designated tactical helicopter and the Air Force's Kaman HH- the L-7, powers the Army's twin engine Grumman 43B "Huskie" rescue helicopter, as well as the Cana OV -1 " Mohawk" high speed observation aircraft dair CL-84 tilt-wing V/ STOL aircraft under devel which has a capability for short field operation.