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I Ngaeronautical Engi :Al _ A ST,_ _-.................. u,;, __2_" °eb?'._sr _ !!%_9 i .eronautical F_,.-cjineed_ng Aeronautical Er ineerir i ngAeronautical Engi :al _. Nineerir Aemnautic. l autic-al Aerona 7 ! ACCESSION NUMBER RANGES Accession numbers cited in this Supplement fall within the following ranges. STAR (N-10000 Series) N89-10001 -- N89-11688 IAA (A-10000 Series) A89-t0001 A89-12760 This bibliography was prepared by the NASA Scientific and Technical Information Facility operated for the National Aeronautics and Space Administration by RMS AssociaTes. NASA SP-7037(236) AERONAUTICAL ENGINEERING A CONTINUING BIBLIOGRAPHY WITH INDEXES (Supplement 236) A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in January 1989 in • Scientific and Technical Aerospace Reports (STAR) v • International Aerospace Abstracts (IAA). Office of Management N_A National Aeronautics and Space Administration Scientific and Technical Information Division Washington, DC 1989 This supplement is available from the National Technical Information Service (NTIS), Springfield, Virginia 22161, price code A06. INTRODUCTION This issue of Aeronautical Engineering -- A Continuing Bibliography (NASA SP-7037) lists 430 reports, journal articles and other documents originally announced in January 1989 in Scientific and Technical Aerospace Reports (STAR) or in International Aerospace Abstracts (IAA). The coverage includes documents on the engineering and theoretical aspects of design, construction, evaluation, testing, operation, and performance of aircraft (including aircraft engines) and associated components, equipment, and systems. It also includes research and development in aerodynamics, aeronautics, and ground support equipment for aeronautical vehicles. Each entry in the bibliography consists of a standard bibliographic citation accompanied in most cases by an abstract. The listing of the entries is arranged by the first nine STAR specific categories and the remaining STAR major categories. This arrangement offers the user the most advantageous breakdown for individual objectives. The citations include the original accession numbers from the respective announcement journals. The IAA items will precede the STAR items within each category Seven indexes -- subject, personal author, corporate source, foreign technology, contract number, report number, and accession number -- are included. An annual cummulative index will be published. Information on the availability of cited publications including addresses of organizations and NTIS price schedules is located at the back of this bibliography. iii TABLE OF CONTENTS Page Category 01 Aeronautics (General) 1 Category 02 Aerodynamics 4 Includes aerodynamics of bodies, combinations, wings, rotors, and control sur- faces; and internal flow in ducts and turbomachinery. Category 03 Air Transportation and Safety 18 Includes passenger and cargo air transport operations; and aircraft accidents. Category 04 Aircraft Communications and Navigation 23 Includes digital and voice communication with aircraft; air navigation systems (satellite and ground based); and air traffic control. Category 05 Aircraft Design, Testing and Performance 25 Includes aircraft simulation technology. Category 06 Aircraft Instrumentation 3O Includes cockpit and cabin display devices; and flight instruments. Category 07 Aircraft Propulsion and Power 33 Includes prime propulsion systems and systems components, e.g., gas turbine engines and compressors; and onboard auxiliary power plants for aircraft. Category 08 Aircraft Stability and Control 38 Includes aircraft handling qualities; piloting; flight controls; and autopilots. Category 09 Research and Support Facilities (Air) 41 Includes airports, hangars and runways; aircraft repair and overhaul facilities; wind tunnels; shock tubes; and aircraft engine test stands. Category 10 Astronautics 42 Includes astronautics (general); astrodynamics; ground support systems and facilities (space); launch vehicles and space vehicles; space transportation; space communications, spacecraft communications, command and tracking; spacecraft design, testing and performance; spacecraft instrumentation; and spacecraft propulsion and power. Category 11 Chemistry and Materials 43 Includes chemistry and materials (general); composite materials; inorganic and physical chemistry; metallic materials; nonmetallic materials; propellants and fuels; and materials processing. II Category 12 Engineering 43 Includes engineering (general); communications and radar; electronics and electrical engineering; fluid mechanics and heat transfer; instrumentation and photography; lasers and masers; mechanical engineering; quality assurance and reliability; and structural mechanics. Category 13 Geosciences 54 Includes geosciences (general); earth resources and remote sensing; energy production and conversion; environment pollution; geophysics; meteorology and climatology; and oceanography. Category 14 Life Sciences 57 Includes life sciences (general); aerospace medicine; behavioral sciences; man/system technology and life support; and space biology. Category 15 Mathematical and Computer Sciences 57 Includes mathematical and computer sciences (general); computer operations and hardware; computer programming and software; computer systems; cybernetics; numerical analysis; statistics and probability; systems analysis; and theoretical mathematics. Category 16 Physics 59 Includes physics (general); acoustics; atomic and molecular physics; nuclear and high-energy physics; optics; plasma physics; solid-state physics; and ther- modynamics and statistical physics. Category 17 Social Sciences B.A. Includes social sciences (general); administration and management; documen- tation and information science; economics and cost analysis; law, political sci- ence, and space policy; and urban technology and transportation. Category 18 Space Sciences N.A, Includes space sciences (general); astronomy; astrophysics; lunar and planet- ary exploration; solar physics; and space radiation. Category 19 General 60 Subject Index ....................................................................................................................... A-1 Personal Author Index ........................................................................................................ B-1 Corporate Source Index ...................................................................................................... C-1 Foreign Technology Index ................................................................................................... D-1 Contract Number Index ....................................................................................................... E-1 Report Number Index .......................................................................................................... F-1 Accession Number Index .................................................................................................... G-1 vi TYPICAL REPORT CITATION AND ABSTRACT NASA SPONSORED 11_-_" ON MICROFICHE ACCESSION NUMBER N89-10029"# North Carolina State Univ., Raleigh. Dept. of _ CORPORATE SOURCE Mechanical and Aerospace Engineering. TITLE -- A TRANSONIC INTERACTIVE BOUNDARY-LAYER THEORY FOR LAMINAR AND TURBULENT FLOW OVER SWEPT WINGS Final Report AUTHORS - SHAWN H. WOODSON and FRED R. DEJARNETTE Washington Oct. 1988 82 p CONTRACT NUMBER-------_ (Contract NCC1-22) _ PUBLICATION DATE REPORT NUMBERS (NASA-CR-4185; NAS 1.26:4185) Avail: NTIS HC A05/MF A01 _ PRICE CODE COSATI CODE CSCL 01A "_ AVAILABILITY SOURCE A 3-D laminar and turbulent boundary-layer method is developed for compressible flow over swept wings. The governing equations and curvature terms are derived in detail for a nonorthogonal, curvilinear coordinate system. Reynolds shear-stress terms are modeled by the Cebeci-Smith eddy-viscosity formulation. The governing equations are descretized using the second-order accurate, predictor-corrector finite-difference technique of Matsuno, which has the advantage that the crossflow difference formulas are formed independent of the sign of the crossflow velocity component. The method is coupled with a full potential wing/body inviscid code (FLO-30) and the inviscid-viscous interaction is performed by updating the original wing surface with the viscous displacement surface calculated by the boundary-layer code. The number of these global iterations ranged from five to twelve depending on Mach number, sweep angle, and angle of attack. Several test cases are computed by this method and the results are compared with another inviscid-viscous interaction method (TAWFIVE) and with experimental data. Author TYPICAL JOURNAL ARTICLE CITATION AND ABSTRACT NASA SPONSORED _ _- ON MICRORCHE ACCE_ON NUMBER-------_ A89-12562"# National Aeronautics and Space Administration. Langley Research Center, Hampton, Va. EFFICIENT VIBRATION MODE ANALYSIS OF AIRCRAFT WITH MULTIPLE EXTERNAL STORE CONFIGURATIONS AUTHOR-_-_ M. KARPEL (NASA, Langley Research Center, Hampton, VA; israel Aircraft Industries, Ltd., Lod) Journal of Aircraft (ISSN 0021-8669),_JOURN/U, TITLE vol. 25, Aug. 1988, p. 747-751. refs A coupling method for efficient vibration mode analysis of aircraft with multiple external store configurations is presented. A set of low-frequency vibration modes, including rigid-body modes, represent the aircraft. Each external store is represented by its vibration modes with clamped boundary conditions,
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