2 edition of Comparative optical measurements of airspeed and aerosols on a DC-8 aircraft found in the catalog.
Comparative optical measurements of airspeed and aerosols on a DC-8 aircraft
by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, DC], Springfield, Va
Written in English
|Statement||Rodney Bogue ... [et al.].|
|Series||NASA technical memorandum -- 107467.|
|Contributions||Bogue, Rodney K., United States. National Aeronautics and Space Administration.|
|The Physical Object|
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Get this from a library. Comparative optical measurements of airspeed and aerosols on a DC-8 aircraft. [Rodney K Bogue; Hugh L. Dryden Flight Research Center.;]. 21st Century Collection of NASA and NACA Dryden Technical Reports: X-Plane, SR, Space Shuttle, Hypersonic Research, Fighter Planes (Two CD-ROM Set) [News, World Spaceflight] on *FREE* shipping on qualifying offers.
21st Century Collection of NASA and NACA Dryden Technical Reports: X-Plane, SR, Space Shuttle, Hypersonic ResearchPrice: $ Comparative optical measurements of airspeed and aerosols on a DC-8 aircraft flight test program on the NASA DC-8 aircraft in November relied on optical backscatter from natural.
We summarise the microphysical and optical parameters of some principal aerosol species obtained by instrumentation on the UK Met Office C aircraft during international field campaigns since Report No. NATURE AND CONTROL OF AIRCRAFT ENGINE EXHAUST EMISSIONS Prepared for the National Air Pollution Control Administration Department of Health, Education, and Welfare (Contract No.
PH) NORTHERN RESEARCH AND ENGINEERING CORPORATION Vassar Street Cambridge, Massachusetts November, Copy No. This banner text can have markup. web; books; video; audio; software; images; Toggle navigation. So at high airspeed, the blades receive a rotational airflow vector determined by engine rpm, and also an airspeed airflow vector determined by aircraft airspeed.
So for any given rpm, the blades will indeed experience a greater airflow speed, when the aircraft flies faster, and therefore may go supersonic as speed increases. Full text of "DTIC ADA Aircraft Icing Handbook. (Update)" See other formats. Measurements from cirrus levels and also in an aircraft contrail (fig.
) may be extrapolated to give likely concentrations in the contrail at high values of supersaturation (>25% water) and to low values to give the concentrations of giant CCN likely to freeze first homogeneously as they dilute at water saturation of above 70% to 90%.
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