Douglas Aircraft

W. C. Robiuson, ed., Eluorine Sjsterms Handbook, Douglas Aircraft Co., Inc., Long Beach, Calif., 1967. 

Potter, D.L. et al.. Primary Adhesive Bonded Structure Technology (PABST) Design Handbook for Adhesive Bonding. Report AFFDL-TR-79-3129, Douglas Aircraft Co., Air Force Flight Development Laboratory (FBA), Air Force Systems Command, WPAFB (November, 1979). 

John Hart-Smith, Douglas Aircraft Company, Long Beach, Caiifomia, personal communication. 

Lake, Percussion Primers, Design Requirements McDonnell Douglas Aircraft Company, Report MDC A0514 (1970) 32) F.J. Valenta, Ef-... 

David E. Kranbuehl appreciates partial support from the NSF Science and Technology Center at Virginia Polytechnic Institute and State University under Contract DMR91-2004, a NASA Langley grant NAGI-23 and support from the Douglas Aircraft Corporation. 

J.R. Henderson, R.A. Willett, M.Muramoto and D.C. Richardson, Table of Hormonic Franck-Condon Overlap Integrals Including Displacement of Normal Coordinates, Douglas Aircraft Co. Report S.M. (1964)45807. 

Shannon, R. W., et al, Primary Adhesively Bonded Structure Technology (PABST) General Materials Property Data, Douglas Aircraft Co., McDonnell Douglas Corp., Air Force Flight Dynamics Laboratory, Technical Report AFFDL-TR-77-107, September 1977. 

Center at Valley Forge, Pa. (9). It was the Library of Congress recommendation for the safety limits of cellulose-type materials which made possible the success of this project and others which have followed. After the St. Louis fire at the Military Records Center, the Library of Congress was again involved in vacuum—air purge drying operations, this time in collaboration with McDonnell Douglas Aircraft Corp. (7). 

Astropower Laboratory, Douglas Aircraft Co., Inc., Newport Beach, Calif. 

Smith, A.M.O. and Gamberoni, N. (1956). Transition, pressure gradient and stability theory. Douglas Aircraft Kept. No. ES-26338. 

D. L. Hildenbrand, Douglas Aircraft Company J. L. Margrave, Rice University... 

Exposure limits have been defined for land, sea and air the National Academy of Sciences gives a 90-day atmospheric limit of 0.05 p.p.m. in submarines, and a Douglas aircraft continuous atmospheric limit of 0.04 p.p.m. [40]. These recommendations exist because of the possibility of producing phosgene as a result of the decomposition of chlorofluorocarbon refrigerants used in air-conditioning systems. 

Question by M. P. Erhard, Douglas Aircraft You mentioned that a decreasing load shows a higher thermal conductivity than an increasing load. Were you able to correlate this with your thickness measurements It appears that this effect might be due to hysteresis wdth the sample not springing back to its original shape. 

Douglas Aircraft Company Santa Monica California... 

J. M. Toth, Jr., Douglas Aircraft Company, Inc., Santa Monica Report SM-42594 (1962). 

Hart-Smith U. Effects of flaws and porosity on strength of adhesive-bonded joints. Douglas Aircraft Co 1981. report DP 7388. 

Upper aft carbon/epoxy rudder program begins on the DC-10 airplane by McDonald Douglas Aircraft Co., CA, USA,... 

JENKINS R K ASTROPOWER LABORATORY DOUGLAS AIRCRAFT CO INC NEWPORT BEACH CALIFORNIA NASA AND CFSTI NASA-CR-96151 SM-49143-S-1 N68-32037 1-70 1968... 

Francis Hettinger Clauser obtained his BS degree in 1934, and the PhD degree in aeronautics in 1937 from Caltech. He was for the next ten years engineer of aerodynamic design with Douglas Aircraft Corp., from 1946 to 1960 then professor of aeronautics and department ehairman at Johns Hopkins University,... 

After having been professor of applied mathematics at Australian National University ANU, Canberra, he took over as professor of applied mechanics and geophysics at University of California, San Diego, in 1965. Miles was chairman of applied mechanics and engineering from 1968 to 1972, and vice-chancellor of academic affairs from 1980 to 1983. During his early career he was a consultant to Northrop Aviation Co., North American Aviation Co., the US Naval Ordnance, Douglas Aircraft Co, or the Aerospace Corp. 

Douglas Aircraft Co., Santa Monica CA, taking then over as professor of engineering science at California Institute of Technology, Pasadena CA, till retirement in 1978. He was in parallel consultant to industrial firms, notably the Naval Ordnance Test Station,... 

C. H. Reynales, "Compatibility of Materials with Oxygen," Propulsion Report No. D81-444, Douglas Aircraft Company, Long Beach, California (October 1, 1958). 

Douglas Aircraft Company, "Anti-Seize Lubricants for Mating Parts," Process Specification No. 1.22, Santa Monica, California (March 27, 1958). 

Question by J. L, Cook, Douglas Aircraft Company Was a deflectometer placed below the platen the only means of measuring the deformation (strain) in the specimen or didyou use some type of attached extensometer on the specimen ... 

Hart-Smith L J (1974b), Analysis and design of advanced composite bonded joints , Hampton, VA, Douglas Aircraft Company, Report no. CR-2218. 

The extensive use of carbon fiber composites in aerospace is illustrated in Fig. 9.1. This figure shows the large number of applications of polymer/carbon-fiber composites in a new passenger plane, the McDonnell-Douglas Aircraft MD-12X. Other new airplanes, such as the Boeing 777 and the Airbus A340, make similar extensive use of these composites. ] The Airbus A340, for instance, incorporates 4000 kg of epoxy-carbon fiber... 

The aviation industry uses a combination of system safety engineering and regulatory compliance. Larson (1989), also from Douglas Aircraft Company, lists the... 

Source T.L Mackay and C.B. Gilpin, Stress Corrosion Cracking of Titanium Alloys at Ambient Temperature in Aqueous Solutions, Missile Space Systems Division, Astropovwer Latxxatory, Douglas Aircraft CompcNiy, ReportNo. SM-49105-F1, June, 1967... 

Comment by E. P. Troeger, Douglas Aircraft Company, Inc, We use an impact machine which is of the type approved by the industry in general. Our results are quantitative. The detonation level we consider as acceptable is the limit of our machine, which is 185 ft-lbs. 

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