Aerodynamically controlled variable area ratio rocket nozzle
Greco, Robert V.
[1959]. 51 leaves.

Aerodynamically controlled variable area ratio rocket nozzle
Higgins, Jerome S.
1959.. 49 leaves.

Aerodynamically controlled variable area ratio rocket nozzle
Whiteman, George.
1959.. 46 leaves.

Aerodynamically induced vibration and noise in circular saw
Cho, Hyung S.
1977. 2 Mikrofiches.

Aerodynamically induced vibration and noise in circular saws
Cho, Hyung Suck.
1977.. 3, xx, 112 leaves.

Aerodynamical properties of an air layer affected by vegetation
Hayashi, Yousay
Ibaraki. Environmental Research Center, Univ. of Tsukuba. 1983. 54 S.. Suiri-jikken-sentÅa <Tsukuba>: Environmental Research Center papers ; 3.

Aerodynamic analyses requiring advanced computers: a conference held at Langley Research Center in Hampton, Virginia on March 4-6, 1975
Washington. National Aeronautics and Space Administration, Scientific and Technical Office ;. 1975.. 2 v. (xi, 1471 p.).

Erläuterungen zu Theodor Storm, Viola Tricolor. Beim Vetter Christian: a conference held at Langley Research Center in Hampton, Virginia on March 4-6, 1975
Eversberg, Gerd
Hollfeld/Obfr.. Bange. 1984. 71 S.. Koenigs Erlaeuterungen und Materilaien. 199.

Aerodynamic analysis and performance prediction of the multipurpose autonomous flight vehicle Jabiru.
Waller, Björn
1994. 67 bl..

Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds
Boppe, Charles W.
[Washington, D.C.]. National Aeronautics and Space Administration, Scientific and Technical Information Branch,. 1987.. 1 v..

Aerodynamic and deployment characteristics of multistage canopy and suspension-line reefing systems for a twin-keel all-flexible parawing
Morgan, Harry L. ; McHatton, Austin D.
Washington . NASA. 1971. 60 S..

Aerodynamic and flow-visualization studies of two delta-wing entry vehicles at a Mach number of 20.3
Arrington, James P. ; Stone, David R.
Washington . NASA. 1973. 70 S..

Aerodynamic and hydrodynamic tests of a family of models of flying-boat hulls derived from a streamline body: NACA model 84 series
Parkinson, J.B. ; Olson, R.E. ; Draley, E.C. ; Luoma, A.A.
Washington . NACA. 1943. 2 Microfiches..

Aerodynamic and hydrodynamic tests of a family of models of flying-boat hulls derived from a streamline body NAC model 84 series,
Parkinson, John Bingham,
Washington, . U. S. Govt. Print. Off., 1943 [i. e.. 1947]. p. cm..

Aerodynamic and related hydrodynamic studies using water facilities: papers presented at the Symposium of the Fluid Dynamics Panel in Monterey, California, United States, 20 - 23 October 1986
Neuilly-sur-Seine. AGARD. 1987. Getr. Zählung. AGARD conference proceedings ; 413.

Aerodynamic and rocket-exhaust heating during launch and ascent.
Springfield, Va.. for sale by the Clearinghouse for Federal Scientific and Technical Information,. 1969.. iv, 29 p. ;.

Aerodynamic capture of particles: proceedings of a symposium held at B.C.U.R.A, Leatherhead, Surrey, 1960
Richardson, E. G.
New York, NY u.a.. Pergamon Pr.. 1960. 200 S. : Ill., graph. Darst..

Aerodynamic capture of particles;: proceedings of a conference held at B.C.U.R.A., Leatherhead, Surrey, 1960.
Richardson, Edward Gick,
New York, . Symposium Publications Division, Pergamon Press,. 1960.. viii, 200 p..

Aerodynamic characteristics at high speeds of related full scale propellers having different blade section cambers
Maynard, Julian D. ; Salters, Leland B.
Washington, DC. U.S. Government Printing Office. 1957. II, 24 S. : Ill., überw. graph. Darst.. Report / National Advisory Committee for Aeronautics ; 1309.

Aerodynamic characteristics at Mach 1.60, 2.00, and 2.50 of a cruciform missile configuration with in-line tail controls
Corlett, W.A. ; Fuller, D.E.
Washington . 1965. 41 p..

Aerodynamic characteristics determined during development of the Apollo launch escape vehicle configuration
Moseley, William C. ; Bowen, Francis Evans
Washington . NASA. 1969. 79 S..

¬The¬ aerodynamic characteristics of a 2 5th scale "finn" sail and its efficiency when sailing to windward
Marchaj, Czeslaw A.
Southampton. 1964. 9, [33] S. : Ill., graph. Darst.. S.U.Y.R. report ; 13.

Aerodynamic characteristics of a five-jet VTOL configuration in the transition speed range
Margason, Richard J. ; Gentry, Garl L.
Washington . National aeronautics and space Administration. 1968. 187 S..

Aerodynamic characteristics of a full-scale fan-in-wing model including results in ground effect with nose-fan pitch control
Kirk, Jerry V. ; Hickey, David H. ; Hall, Leo P.
Washington . National Aeronautics and Space Administration. 1964. 145 S..

Aerodynamic characteristics of a hypersonic research airplane concept having a 70À swept double-delta wing at Mach numbers from 2.50 to 2.86
Penland, Jim A. ; Fournier, Roger H. ; Marcum, Don C.
Washington . 1975. 81 p..

¬The¬ aerodynamic characteristics of airfoils as affected by surface roughness
Hocker, Ray W.
Washington, DC. National Advisory Committee for Aeronautics. 1933. 10 S., [10] Bl.. Technical note ; 457.

Aerodynamic characteristics of a large aircraft to transport space shuttle orbiter or other external payloads
Paulson, J.W.
Washington . 1975. 62 p..

Aerodynamic characteristics of a large-scale model with an unswept wing and augmented jet flap
Koenig, David G. ; Corsiglia, Victor R. ; Morelli, Joseph P.
Washington . National aeronautics and space Administration. 1968. 89 S..

Aerodynamic characteristics of a large-scale V/STOL transport model with lift and lift-cruise fans
Hall, Leo P. ; Hickey, David H. ; Kirk, Jerry V.
Washington . National aeronautics and space Administration. 1967. 86 S..

Aerodynamic characteristics of an all-body hypersonic aircraft configuration at Mach numbers from 0.65 to 10.6
Nelms, Walter P. ; Thomas, Charles L.
Washington, DC. National Aeronautics and Space Administration. 1971. V, 93 S.. NASA technical note : D ; 6577.

Aerodynamic characteristics of a powered, externally blown flap STOL transport model with two engine simulator sizes
Johnson, W.G.
Washington . 1975. 291 p..

Aerodynamic Characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes
Rieb, John M.
[Washington]. [The Superintendent of Documents]. 1953. 19 S. ; 4-o. Report / National Advisory Committee for Aeronautics ; 1144.

Aerodynamic characteristics of a refined deep step planing tail flying boat hull with various forebody and afterbody shapes
Riebe, John M. ; Naeseth, Rodger L.
Washington, DC. U.S. Government Printing Office. 1953. 19 S. : Ill., graph. Darst.. Report / National Advisory Committee for Aeronautics ; 1144.

Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations
Hayes, Clyde.
Washington, D.C.. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;. 1983.. 360 p..

Aerodynamic characteristics of a series of twin-inlet air-breathing missile configurations
Hayes, Clyde.
Washington, D.C.. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;. 1983-. 3 v..

Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86
Stallings, Robert L.
Washington, D.C.. National Aeronautics and Space Administration, Scientific and Technical Information Office ;. 1981.. 26 p..

Aerodynamic characteristics of a swept-wing cruise missile at Mach numbers from 0.50 to 2.86
Spearman, M. Leroy ; Collins, Ida K.
Washington . 1972. 40 S..

Aerodynamic characteristics of atmospheric boundary layers
Plate, Erich J.
Oak Ridge, Tenn.. US Atomic Energy Comm., Office for Information Services. 1972. VIII, 190 S. : graph. Darst..

Aerodynamic characteristics of a tubeflight vehicle support system
Duffy, Robert E. ; Cooke, George C.
Troy, N.Y.. Rensselaer Polytechnic Institute,. [1968]. 46, 66 leaves.

Aerodynamic characteristics of a vane flow angularity sensor system capable of measuring flightpath accelerations for the Mach number range from 0.40 to 2.54
Sakamoto, Glenn M.
Washington . NASA. 1976. 43 p..

Aerodynamic characteristics of controls: Papers pres. and Discussions
Neuilly-sur-Seine, France. 1979. 300 S.. AGARD Conference Proceedings ; 262.
ISBN 92-835-0252-3

Aerodynamic characteristics of controls: papers presented and discussions held at the Fluid Dynamics Panel Symposium held at the Italian Air Force Academy, Pozzuoli, Italy, 14-17 May, 1979.
Neuilly-sur-Seine, France. AGARD,. 1979.. 520 p. in various pagings.

Aerodynamic characteristics of the close-coupled canard as applied to low-to-moderate swept wings: final report, 1970-1974
Lacey, D.W.
Springfield - Va. . 1979-. vol.1-3-.

<<The>> aerodynamic characteristics of the jet wing and its application to high speed aircraft
Alexander, A.J.
Cranfield . 1961. 3 Mikrofiches.

Aerodynamic characteristics of the sharp right circular cone at Mach 20.3 and angles of attack to 110À in helium
Maddalon, Dal V.
Washington . National aeronautics and space Administration. 1966. 52 S..

Aerodynamic characteristics of two rotorcraft airfoils designed for application to the inboard region of a main rotor blade
Noonan, Kevin W.
Washington, D.C.. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;. 1990.. 86 p..

Aerodynamic characteristics of vehicle bodies at crosswind conditions in ground proximity
Grunwald, Kalman J.
Washington, DC. National Aeronautics and Space Administration. 1970. 140 S.. NASA technical note ; D-5935.

Aerodynamic components of aircraft at high speeds
Donovan, Allen F.
Princeton, NJ. Univ. Pr.. 1957. XIV, 845 S. : graph. Darst.. High speed aerodynamics and jet propulsion. ; 7..

Aerodynamic considerations of F1 race car design
Purnell, Anthony John.
c1983.. 213 [i.e. 215] leaves.

Aerodynamic control of a vehicle with flexible longitudinal mode
Walters, Edward Kenneth.
c1993.. 148 leaves.

Aerodynamic control of nitrogen oxides and other pollutants from fossil fuel combustion
Shoffstall, D. R. ; Larson, D. H.
Springfield, Va.. NTIS, National Technical Information Service.

Aerodynamic damping and buffet response of an aeroelastic model of the Saturn I Block II launch vehicle
Hanson, Perry W. ; Doggett, Robert V.
Washington . National aeronautics and space Administration. 1965. 53 S..

Aerodynamic data accuracy and quality: requirements and capabilities in wind tunnel testing ; papers presented and discussions held at the symposium of the Fluid Dynamics Panel in Naples, Italy, 28. September - 1. October 1987
Neuilly-sur-Seine. 1988. Getr. Zählung. Agard conference proceedings ; 429.
ISBN 92-835-0469-0

Standard operating procedures and organization of German Phase I, II, and III Study Groups, New Drug Development Group (AWO), and Study Group of Pharmacology in Oncology and Hematology (APOH) of the Association for Medical Oncology (AIO) of the German Cancer Society: requirements and capabilities in wind tunnel testing ; papers presented at the Symposium of the Fluid Dynamics Panel in Naples, It202 5290200-6
Basel ¬[u.a.]¬. Karger. 1998. VI, 70 S. : graph. Darst.. Onkologie ; 21, Suppl. 3.
ISBN 3-8055-6742-1

Aerodynamic data accuracy and quality: requirements and capabilities in wind tunnel testing: Papers and discussions
Neuilly-sur-Seine, France. 1988. ca.530 S.. AGARD Conference Proceedings ; 429.
ISBN 92-835-0469-0

Aerodynamic data on a large semispan tilting wing with 0.5-diameter chord, double-slotted flap, and both left- and right-hand rotation of a single propeller
Fink, Marvin P. ; Mitchell, Robert G. ; White, Lucy C.
Washington . National aeronautics and space Administration. 1966. 119 S..

Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a double-slotted flap and left- and right-hand rotation of a single propeller in presence of fuselage
Fink, Marvin P.
Washington . 1966. 119 S..

Aerodynamic data on a large semispan tilting wing with a 0.5-diameter chord, a single-slotted flap, and both left- and right-hand rotation of a single propeller
Fink, Marvin P. ; Mitchell, Robert G.
Washington . National aeronautics and space Administration. 1967. 157 S..

Aerodynamic data on large semispan tilting wing with 0.6-diameter chord, single-slotted flap, and single propeller rotating down at tip
Fink, Marvin P. ; Mitchell, Robert G. ; White, Lucy C.
Washington . National Aeronautics and Space Administration. 1964. 144 S..

¬The¬ aerodynamic Derivatives with respect to sideslip for a delta wing with small dihedral at zero incidence at supersonic speeds
Robinson, A
1952.

¬The¬ aerodynamic derivatives with respect to sideslip for a delta wing with small dihedral at zero incidence at supersonic speeds
Taylor, Arthur ; Hunter-Tod, John Hunter
London. His Majesty's Stationery Office. 1947 [erschienen] 1952. 14 S. : graph. Darst.. Reports and memoranda / Aeronautical Research Council, London ; 2410.

Aerodynamic design an doptimisation of flight vehicles in a concurrent multi-disciplinary environment
[Elektronische Ressource]. Neuilly-sur-Seine. North Atlantic Treaty Organization, Research and Technology Organization. 2000. RTO meeting proceedings ; 35.

Aerodynamic design and optimization of intermediate ducts for high by-pass ratio jet engines
Wallin, Fredrik
Göteborg. Chalmers tekniska högskola,. 2006. xiii, 22 s..

Aerodynamic design for supersonic flight: 19th April 1988 ; one day symposium
London. 1988. 204 S..

The aerodynamic design of aircraft: a detailed introduction of the current aerodynamic knowledge and practical guide to the solution of aircraft design problems
Küchemann, Dietrich
repr. of the Pergamon ed. 1978. Elkins Park, Pa.. Franklin Book. 1993. X, 564 S.. Pergamon international library of science, technology, engineering, and social studies.
ISBN 0-08-020515-1

The aerodynamic design of aircraft: a detailed introductionto the current aerodynamic knowledge and practical guide to the solution of aircraft design problems
Küchemann, Dietrich
1. ed. Oxford. Pergamon Press. 1978. X, 564 S.. Pergamon international library of science, technology, engineering, and social studies.
ISBN 0-08-020515-1 (hardc.)

<<The>> aerodynamic design of blower tunnels with wide-angle diffusers
Mehta, R.D.
Oxford a.o. . Pergamon Press. 1977. 62 p..

<<The>> aerodynamic design of hypersonic contoured axisymmetric nozzles including real gas effects
Simeonides, G.
Rhode Saint Genèse . Von Karman Institute for Fluid Dynamics. 1987. 51 S..

Aerodynamic design of supersonic nozzles using the method of characteristics
Weinmann
Stuttgart .

The aerodynamic design of the oblique flying wing supersonic transport
Van der Velden, Alexander J. M. ; Kroo, Ilan.
Palo Alto, Calif.. Stanford University ;. [1990]. 1 v..

The aerodynamic design optimisation of a forward swept wing fighter aircraft
Cook, M. V. ; Heydari, F.
1987. 37 Bl.. Cranfield College of Aeronautics report ; 8718.
ISBN 0-947767-83-5

Aerodynamic development of the X-31 aircraft for the high angle of attack region
Kraus, Werner
München. Zentrale Berichtsstelle, Technisch-wissenschaftliche Information, Messerschmitt-Bölkow-Blohm GmbH. 1991. 35 S.. MBB-S-PUB ; 452.

¬The¬ aerodynamic diameter and specific surface area of branched chain-like aggregates
Kops, Joannes Arnoldus Marcus Maria
1976. 119 S..

¬The¬ aerodynamic drag
Graf, Walter H. ; Prost, J.-P.
Lausanne. EPFL. 1980. Getr. Zählung. Laboratoire d'Hydraulique <Lausanne>: Communication du ... . ; 42..

Aerodynamic drag mechanisms of bluff bodies and road vehicles: [proceedings of the Symposium on Aerodynamic Drag Mechanisms of Bluff Bodies and Road Vehicles held at the General Motors Research Laboratories, Warren, Mich., Sept. 27-28, 1976]
Sovran, Gino ¬[Hrsg.]¬
New York. Plenum Pr.. 1978. XI, 380 S..
ISBN 0-306-31119-4

Aerodynamic drag on a vehicle in a tube.
Nwude, Joseph Kanayo.
1966.. [9], 58 leaves.

Aerodynamic drag reduction technologies: proceedings of the CEAS/DragNet European Drag Reduction Conference, 19 - 21 June 2000, Potsdam, Germany
Thiede, Peter
Berlin [u.a.]. Springer. 2001. XII, 390 S.. Notes on numerical fluid mechanics ; 76.
ISBN 3-540-41911-X alk. paper

The aerodynamic effect of fillet radius in a low speed compressor cascade
Curlett, Brian P.
[Washington, DC]. National Aeronautics and Space Administration ;. 1992]. 1 v..

¬The¬ aerodynamic Effect of ground proximity on lateral control of slender aircraft in the landing approach
Pinsker, W. J. G.
London. Her Majesty's Stationery office. 1971. 17 S. &434 Ill. ; 4-o. Current Papers / Ministry of Aviation Supply. Aeronautical Research Council ; No 1152.

Aerodynamic effects of a reverse jet on a wing and nacelle
Martin, Arnold Woods. ; Myers, Harry S.
1947.. 41, [44] leaves.

¬The¬ aerodynamic effects of aspect ratio on control surface flutter
Hall, H. ; Chapple, E. W.
London. Her Majesty's Stationery Office. 1959. 8 S., 4 Bl.. Current Papers / Ministry of Supply, Aeronautical Research Council ; 434.

The aerodynamic effects of high-speed trains on people and property at stations in the Northeast Corridor: safety of high-speed ground transportation systems
Washington, D.C.. U.S. Dept. of Transportation, Federal Railroad Administration, Office of Research and Development,. 1999.. 1 v. (various pagings).

Aerodynamic effects of tip clearance in a lifting line in a non-uniform flow
Sugiyama, Yoshiyuki
Göttingen . 1973. 33 Bl..

Aerodynamic engine, airframe integration for high performance aircraft and missiles: papers presented and discussions held at the Fluid Dynamics Panel Symposium held in Fort Worth, Texas, United States, 7th-10th October 1991
Neuilly sur Seine. 1992. Getr. Zählung : Ill., graph. Darst.. AGARD conference proceedings ; 498.
ISBN 92-835-0672-3

1977. 182 S..
ISBN 0-207-13517-7

Aerodynamic evaluation of a small transonic axial compressor
Eriksson Alvbring, Johan
Göteborg. Chalmers tekniska högsk.,. 2005. iv, 74 s..

Aerodynamic evaluation of two compact radial inflow turbine rotors
Simonyi, P. Susan
Cleveland, Ohio. Lewis Research Center. 1995. 68 S. : Ill., graph. Darst..

Aerodynamic flow field measurements for automotive systems
Hepner, Timothy E.
Hampton, Va.. National Aeronautics and Space Administration, Langley Research Center ;. 1999]. 1 v..

Aerodynamic flow visualization techniques and procedures: SAE information report
Warrendale, Pa.. SAE. 1986. 59 S.. SAE handbook : Supplement ; 1566.
ISBN 0-89883-418-X

Aerodynamic force-field analysis of a single-stage turbine
Anderson, Steven J.
c1986.. 75 leaves.

Aerodynamic forces and loadings on symmetrical circular arc airfoils with plain leading edge and plain trailing edge flaps
Cahill, Jones F.
Washington, DC. U.S. Government Printing Office. 1953. 38 S. : Ill., graph. Darst.. Report / National Advisory Committee for Aeronautics ; 1146.

Aerodynamic forces on a combination of a wing and a fin oscillating in subsonic flow.
Stark, Valter J. E.,
Linköping, . 1964 ; . 36 s..

Aerodynamic forces on biconvex aerofoils oscillating in a supersonic airstream
Jones, William P. ; Skan, Sylvia W.
London. His Majesty's Stat. Office. 1951 [erschienen] 1953. 34 S.. : graph. Darst.. Reports and memoranda / Aeronautical Research Council, London ; 2749.

Aerodynamic forces on motor vehicles: citations from the NTIS data base
Habercom, G.E.
Springfield - Va. . 1976. 1 Microfiche..

Aerodynamic forces on oscillating low aspect ratio wings in compressible flow.
Merbt, H. ; Landahl, M.
Stockholm. [Inst.],. 1953. 20s.

Aerodynamic forces on rectangular wings oscillating in subsonic flow.
Stark, Valter J. E.,
Linköping, . 1960. 29 s..

Aerodynamic forces on truck models including two trucks in tandem
Hammache, Mustapha, ; Michaelian, Mark. ; Browand, Fred.
Berkeley, Calif.. California PATH Program, Institute of Transportation Studies, University of California at Berkeley,. [2001]. 23 p..

Aerodynamic heating and loading within large open cavities in cone and cone-cylinder-flare models at Mach 6.7
Hunt, L. Roane
Washington, DC. National Aeronautics and Space Administration. 1973. 54 S.. NASA technical note : D ; 7403.

Aerodynamic heating and thermal protection systems: technical papers selected from AIAA 15. Aerospace Sciences Meeting, January 1977, and the AIAA 12. Thermophysics Conference, June 1977
Fletcher, Leroy S. ¬[Hrsg.]¬
Ner York, N.Y.. American Inst. of Aeronautics and Astronautics. 1978. XVII, 449 S. : Ill., graph. Darst.. Progress in astronautics and aeronautics ; 59.
ISBN 0-915928-23-X

Aerodynamic heating and thermal protection systems: technical papers from AIAA 15th Aerospace Sciences Meeting, Jan. 1977, and the AIAA 12th Thermophysics Conference, June 1977
Fletcher, Leroy S. ¬[Hrsg.]¬
New York, NY. 1978. XVI, 424 S. : graph. Darst.. Progress in astronautics and aeronautics ; 59.
ISBN 0-915928-23-X

Aerodynamic heating as shown by temperature-sensitive paints.
Newton, Mass.. The Center ; released by Encyclopaedia Britannica Educational Corp.,. 1968.. 1 cartridge, 4 min..

Aerodynamic heating in the vicinity of corners at hypersonic speeds
Stainback, P. Calvin ; Weinstein, Leonard M.
Washington, DC. National Aeronautics and Space Administration. 1967. 25 S.. NASA technical note : D ; 4130.

Aerodynamic heating of high-speed flywheels in low-density environments
Baer, Melvin R.
Springfield, VA . NTIS. 1978. 1 Mikrofiche.

Aerodynamic heating to the gaps and surfaces of simulated reusable-surface-insulation tile arrays in turbulent flow at Mach 6.6
Weinstein, Irving ; Avery, Don E. ; Chapman, Andrew J.
Washington . 1975. 51 p..

Aerodynamic heating to the Grumman space shuttle orbiters, ROS-NB 1 and ROS-WB 1, at Mach Number 8.0
New Orleans, La. . Chrysler Corp.. 1971. 2 Microfiches.

Aerodynamic influences on the performance of room-sealed appliances.: Les influences aérodynamiques sur le fonctionnement des appareils à tirage équilibré. Aerodynamische Einflüsse auf die Leistung von Geräten mit geschlossenem Verbrennungsraum
Brady, Kenneth John Dudley. ; Dance, E. W. G.,
[Bruxelles] . International Gas Union,. 1967.. 28 p..

Aerodynamic Inputs for problems in aircraft dynamics
Rhode Saint Genèse, Belgium.

Aerodynamic inputs for problems in aircraft dynamics, April 25-29, 1977.
[Rhode-Saint-Genèse, Belgium]. Von Karman Institute for Fluid Dynamics,. 1977.. 2 v..

Aerodynamic Interference: these papers were pres. at the Fluid Dynamics Panel specialists' meeting held in Silver Springs, Md. 28. - 30.9.1970
[Neuilly-sur-Seine]. 1970. Getr. Pag. ; 4-o. AGARD Conference Proceedings ; No. 71.

Aerodynamic Interference: papers pres. at the Fluid Dynamics Panel specialists' meeting, Silver Spring - Md., 28-30 Sept. 1970
Paris . AGARD. 1971. 7 Microfiches.

Aerodynamic interference;: papers presented at a Specialists' Meeting of the Fluid Dynamics Panel of AGARD held in Silver Springs, Md., USA, 28-30 September 1970
[Paris, . North Atlantic Treaty Organization,. 1970]. 1 v. (various pagings).

Aerodynamic interference;: papers presented at the Fluid Dynamics Panel Specialists' Meeting held in Silver Springs, Md., USA, 28-30n September 1970.
[Neuilly-sur-Seine, France] . Advisory Group for Aerospace Research & Development, North Atlantic Treaty Organization,. [1971]. 1 v. (various pagings).

Aerodynamic interference effects caused by parallel-staged simple aerodynamic configurations at Mach numbers of 3 and 6
Decker, John P.
Washington . NASA. 1969. 85 S..

Aerodynamic Interference induced by reaction controls
Spaid, F W
1973.

Aerodynamic interference of high speed ground vehicles
Johnston, G. W. ; Seshagiri, B. V. ; Ellis, N. D.
[Toronto, Ont.]. Institute for Aerospace Studies, University of Toronto. 19761850.

Statistical Geometry of some dense random packing of hard spheres model structures
Takács, L.
Budapest. ....

Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
Lin, Jensen. ; Iliff, Kenneth W.
Edwards, Calif.. National Aeronautics and Space Administration, Dryden Flight Research Center ;. 2000]. 1 v..

Aerodynamic loads on deployed canard surfaces and rocket nose section of the Apollo launch escape vehicle
Moseley, William C. ; Phillips, Branch S.
Washington . NASA. 1969. 81 S..

Aerodynamic noise: proceedings of AROSR-UTIAS Symposium hel at Toronto, 20. - 21. May 1968
Toronto. Univ. Pr.. 1969. 442 S. : Ill..

Aerodynamic noise: proceedings of AFOSR-UTIAS Symposium, held at Toronto, 20-21 May 1968
[Toronto]. University of Toronto Press. 1969. 442 p..
ISBN 0-08-201651-0 : 15.00

Aerodynamic noise.
Neuilly sur Seine, France. North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development,. 1977.. 316 p. in various pagings.

Aerodynamic noise of highspeed railway cars
Moritoh, Yoshio. ; Zenda, Yasuo.
p. 5-9.

Aerodynamic noise radiating from a windbreak cover on a car roof
Sagawa, A. ; Maebashi, E. ; Matsuo, J.
p. 127-130.

Aerodynamic optimisation of h5 1966
Cardamone, Pasquale
1 Schallpl. Unsere neue Musik ; 15.

Aerodynamic optimisation of highly loaded turbine cascade blades for heavy duty gas turbine applications
Cardamone, Pasquale
Als Ms. gedr.. Düsseldorf. VDI-Verl.. 2006. XIII, 136 S. : Ill., graph. Darst.. Fortschritt-Berichte VDI : Reihe 7, Strömungstechnik ; 479.
ISBN 3-18-347907-9

Aerodynamic optimisation of highly loaded turbine cascade blades for heavy duty gas turbine applications: AG Turbo II, Vorhabengruppe 2.3: Strömungen in Turbinen, Vorhaben 2.3.8A: Optimierung von hochbelasteten Turbinenbeschaufelungen für den hohen Reynoldszahlbereich - Schaufelgittermessungen, Analyse ; Abschlussbericht
Cardamone, Pasquale ; Fottner, Leonard
[Neubiberg]. 2005. XIV, 132 S.. Institutsbericht : LRT-WE-12 ; 2005,3.

Aerodynamic Penalties of heavy rain on a landing aircraft
Haines, P A
1982.

Aerodynamic performance and heat transfer characteristics of high pressure ratio transonic turbines.
Demuren, Harold Olusegun.
1976.. 239 leaves.