Scientific and Technical Aerospace Reports, Volume 10NASA, Office of Scientific and Technical Information, 1972 - Aeronautics Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database. |
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Page 1
... wind tunnel tests on slender cones are presented . Tests were made using Mach numbers 7 and 20 , and Reynolds number from 1000 to 10,000 per cm . The study includes flow field , pressure , heat transfer , and force measurements . The ...
... wind tunnel tests on slender cones are presented . Tests were made using Mach numbers 7 and 20 , and Reynolds number from 1000 to 10,000 per cm . The study includes flow field , pressure , heat transfer , and force measurements . The ...
Page 2
... WIND TUNNEL W. Geissler ( DFVLR , Goettingen , West Ger . ) 22 p refs ( See N72-10012 01-02 ) 9. INVESTIGATIONS OF EXHAUST JETS OF TL - ENGINE MODELS E. Schwantes ( DFVLR , Brunswick ) 33 prefs ( See N72-10013 01-28 ) 10. CALCULATION OF ...
... WIND TUNNEL W. Geissler ( DFVLR , Goettingen , West Ger . ) 22 p refs ( See N72-10012 01-02 ) 9. INVESTIGATIONS OF EXHAUST JETS OF TL - ENGINE MODELS E. Schwantes ( DFVLR , Brunswick ) 33 prefs ( See N72-10013 01-28 ) 10. CALCULATION OF ...
Page 3
... wind tunnel balance did not measure jet thrust . A simple determination of jet interference was possible with this arrangement . The jet decreased wing lift , for the ratio of jet velocity and free stream velocity from 2 to 17 the lift ...
... wind tunnel balance did not measure jet thrust . A simple determination of jet interference was possible with this arrangement . The jet decreased wing lift , for the ratio of jet velocity and free stream velocity from 2 to 17 the lift ...
Page 4
... WIND TUNNEL STUDY OF THE WIND LOADING ON A MODEL COOLING TOWER OF IGLOO ( CIRCULAR ARC GENERATOR ) FORM R. W. F. Gould and W. G. Raymer May 1970 12 p refs ( NPL - AERO - SR - 040 ) Avail : NTIS The surface pressure distribution was ...
... WIND TUNNEL STUDY OF THE WIND LOADING ON A MODEL COOLING TOWER OF IGLOO ( CIRCULAR ARC GENERATOR ) FORM R. W. F. Gould and W. G. Raymer May 1970 12 p refs ( NPL - AERO - SR - 040 ) Avail : NTIS The surface pressure distribution was ...
Page 5
... wind tunnel . Measurements for the finless missile were taken at wind tunnel speeds of 70 and 100 m.p.h. and at angles of attack of 10 , 15 , 20 degrees . The planar and cruciform missile measurements were taken at wind tunnel speeds of ...
... wind tunnel . Measurements for the finless missile were taken at wind tunnel speeds of 70 and 100 m.p.h. and at angles of attack of 10 , 15 , 20 degrees . The planar and cruciform missile measurements were taken at wind tunnel speeds of ...
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Abstr AEC Depository Libraries Aerodynamics Aeronautics and Space AGARD aircraft alloys analysis applications Atomic Author GRA Author NSA Avail Boston Spa Boston Spa England boundary layer calculated Calif components density Dept described determined developed discussed Earth Tides effects electric electron energy Engineering equations ESRO evaluation experimental field Final Report flow frequency fuel function Gemini Program Goddard Space Flight Gum Nebula heat Includes Inst investigated magnetic measurements mechanical method Microfilms Order NASA National Aeronautics NLL photocopy coupons NTIS CSCL NTIS HC nuclear obtained Ohio operation parameters particles Ph.D plasma prefs presented pressure problems Proj radiation reactor refs Contract refs Transl Research Reynolds number Royal Aircraft Establishment simulation solar solar cells Space Administration Space Flight Center Spacecraft Center structure surface Tech techniques temperature thermal Thesis transonic Univ velocity Washington West Germany wind tunnel Wright-Patterson AFB
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Page 265 - ... Avail: Univ. Microfilms. Documents so indicated are dissertations selected from Dissertation Abstracts and are sold by University Microfilms as xerographic copy (HC) at $10.00 each and microfilm at $4.00 each, regardless of the length of the manuscript.
Page 265 - STAR is a comprehensive abstracting and indexing journal covering current worldwide report literature on the science and technology of space and aeronautics.
Page 265 - Library also has available many of the non-NASA publications cited in STAR. European requesters may purchase facsimile copy or microfiche of NASA and NASA-sponsored documents, those identified by both the symbols "§
Page 146 - Luftfahrtdokumentation und -Information, Munich. Federal Republic of Germany, at the price shown in deutschmarks (DM). Avail: Issuing Activity, or Corporate Author, or no indication of availability: Inquiries as to the availability of these documents should be addressed to the organization shown in the citation as the corporate author of the document. Avail: US Patent Office.
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Page iv - STAR with the ft symbol. (2) NASA reports only (identified by an asterisk (*)). (3) NASA-accessioned non-NASA reports only (for those who wish to maintain an integrated microfiche file of aerospace documents by the "N...
Page 146 - December. 1964) published by the Committee on Scientific and Technical Information of the Federal Council for Science and Technology...
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Page iv - Avail: Univ. Microfilms. Documents so indicated are dissertations selected from Dissertation Abstracts and are sold by University Microfilms as xerographic copy (HC) and microfilm. All requests should cite the author and the Order Number as they appear in the citation. Avail: US Patent and Trademark Office.
Page 146 - EUROPEAN An extensive collection of NASA and NASA-sponsored publications is maintained by the British Library Lending Division. Boston Spa, Wetherby, Yorkshire. England. By virtue of arrangements other than with NASA, the British Library Lending Division also has available many of the non-NASA publications cited in STAR.