Katz et al., 1982 - Google Patents

Cooling Air Inlet and Exit Geometries on Aircraft Engine Installations

Katz et al., 1982

View PDF
Document ID
345153827970696400
Author
Katz J
Corsiglia V
Barlow P
Publication year
Publication venue
Journal of Aircraft

External Links

Snippet

THE airborne piston engine cooling problem is almost as old as powered flight itself. During World War II, there were numerous studies of engine cooling and nacelle installations. A summary of the British effort at that time is given in Ref. 1. The combined study of engine …
Continue reading at ntrs.nasa.gov (PDF) (other versions)

Classifications

    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies
    • Y02T50/67—Relevant aircraft propulsion technologies
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y02T50/16—Drag reduction by influencing airflow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for

Similar Documents

Publication Publication Date Title
US4449681A (en) Aerodynamically contoured, low drag wing, engine and engine nacelle combination
US5443230A (en) Aircraft wing/nacelle combination
US4629147A (en) Over-the-wing propeller
US4449682A (en) Aerodynamically contoured, low drag wing, engine and engine nacelle combination
US4860976A (en) Attached jet spanwise blowing lift augmentation system
Hawkins YF-16 inlet design and performance
Katz et al. Cooling Air Inlet and Exit Geometries on Aircraft Engine Installations
Kosin Laminar flow control by suction as applied to the x-21a airplane
US3465990A (en) Aircraft having energy-conserving means
Rettie et al. Design and development of an air intake for a supersonic transport aircraft.
Katz et al. AIAA80-1242R
Katz et al. Study of cooling air inlet and exit geometries for horizontally opposed piston aircraft engines
Carson Jr et al. Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20
Hasel The performance of conical supersonic scoop inlets on circular fuselages
Seddon Air intakes for aircraft gas turbines
Harvell et al. Aerodynamic characteristics of a circulation control elliptical airfoil with two blown jets
Coe Review of Drag Cleanup Tests in Langley Full-Scale Tunnel (From 1935 to 1945) Applicable to Current General Aviation Airplanes
Patterson The Design of Aeroplane Ducts: Rules to be Followed for the Reduction of Internal and External Drag
Hickey V/STOL aerodynamics: A review of the technology
LAVI et al. Feasibility investigation of aerodynamic round-lip inlet.
Douglass Aerodynamic installation of high-bypass-ratio fan engines
Henderson Airframe/propulsion integration at transonic speeds
Luskin et al. High-Speed Aerodynamic Problems of Turbojet Installations
Gibson New developments in blown flap noise technology
Elsaadawy et al. Effect of propeller slipstream on heat-exchanger installations at low Reynolds number