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词条 Muniz M-5
释义

  1. Design and development

  2. Specifications

  3. References

name=Muniz M-5 image= caption=

}}{{Infobox Aircraft Type

type=Two/three seat tourer or liaison aircraft national origin=France manufacturer=Société des Avions Caudron designer=Antonio Guedez Muniz first flight=10 July 1930 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Muniz M-5 was the first of Antonio Guedez Muniz's aircraft designs to fly; soon afterwards he became the first Brazilian to design an aircraft which reached series production. The sole example of the M-5, built while he was a student in France by Caudron, was a low wing cabin tourer or military liaison aircraft.

Design and development

Antonio Gedez Muniz was a pioneer of the Brazilian aviation industry but he produced his first designs while at the French Ecole Supérieure de Aéronautique. Several studies remained unbuilt before he had the M-5, a two- or three-seat cantilever low wing cabin tourer, built by the Caudron company.[1][2]

Its wing was straight-tapered in plan out to rounded tips and had an aspect ratio of 8.0, quite high for the time. It had a reflex (double-curved underside) section, 2° of dihedral and thinned continuously to the tips. The wing was built in three parts, with a short, rectangular inner section within the fuselage and two dominant, tapering outer panels. Each outer panel was built around a spruce box spar and the wing surface ahead of it was plywood, forming a torsion resisting D-box. Behind the spar the wing had fabric covering. The M-5's ailerons were long and narrow.[1]

Its rectangular section fuselage was entirely wooden, with spruce longerons and {{convert|2|mm|in|abbr=on|2}} thick plywood covering. The engine was a water-cooled, six cylinder Hispano-Suiza 6Pa with its fuel tanks between the wing spar of the central section, within the lower fuselage. Behind the engine was a multi-windowed cabin with two seats in tandem and fitted with dual controls; without dual control a third tandem seat could be added. The empennage was also wood-framed, with ply-covered fixed surfaces and fabric-covered control surfaces. Like the wings, the tail surfaces were straight-tapered to rounded tips. The tailplane was mounted on top of the fuselage and the elevators were split to allow rudder movement.[1]

The M-5's fixed, tailskid undercarriage had a track of {{convert|2.40|m|ftin|abbr=on}}. Its mainwheels were on cranked steel axles hinged on the lower fuselage longerons which also mounted oblique drag struts, forming a V. Vertical legs from the axle ends operated rubber shock absorbers within the wing leading edge, like those used by Klemm light aircraft.[1]

Muniz had hoped that the aircraft would be ready for the August 1929 International Lightplane Tour of Europe[6] but, though in that month the M-5 was reported as "nearly ready",[1] the first flight was not made for almost another year, when it was flown from Issy-les-Moulineaux on 10 July 1930, piloted by Delmotte. Two days later he flew it to Villacoublay, where five days later Muniz displayed it to the Brazilian community. There were several senior military officers there, as the M-5 could be used as a liaison aircraft. After more flights into early August, the initial report was that the M-5 was stable, fast and landed slowly.[8]

It was still undergoing trials at Villacoublay at the start of 1931.[9] Fifteen months later Muniz had returned to Brazil[10] where he went on to design successful trainers like the Muniz M-7 and M-9; it is not known if the M-5 returned with him.

Specifications

{{Aircraft specs
|ref=Les Ailes August, 1929[1]
|prime units?=met


|genhide=
|crew=One
|capacity=one or two passengers
|length m=7.21
|length note=
|span m=12
|span note=
|height m=2.31
|height note=
|wing area sqm=18
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=450
|empty weight note=
|gross weight kg=
|gross weight lb=
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|max takeoff weight kg=
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|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Hispano 6Pa
|eng1 type=6-cylinder, liquid cooled inline
|eng1 hp=100
|eng1 note=nominal power; continuous rating {{convert|145|hp|kW|abbr=on|order=flip}}
|power original=
|more power=
|prop blade number=2
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=


|perfhide=
|max speed kmh=205
|max speed note=at ground level
|cruise speed kmh=185
|cruise speed note=
|stall speed kmh=65
|stall speed note=minimum speed at ground level
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|minimum control speed kmh=
|minimum control speed mph=
|minimum control speed kts=
|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=5 h
|ceiling m=6500
|ceiling note=absolute
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
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|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
}}

References

1. ^{{cite book |title=World History of Design|volume=2|last=Margolin |first=Victor|year=2015|publisher=Bloomsbury Academic Publications |location=London|isbn=978-1-4725-6651-5|page=497|url=https://books.google.co.uk/books?id=HepgBwAAQBAJ&pg=PA498&lpg=PA498&dq=Muniz+aircraft&source=bl&ots=x1H1yRA13e&sig=u-0J6Flx4v9FuCpcpnTUkU--cKs&hl=en&sa=X&ved=0ahUKEwj6wJDn6abWAhVBBMAKHch3B4Q4ChDoAQglMAA#v=onepage&q=Muniz%20aircraft&f=false }}
2. ^{{cite journal |last=Frachet |first=André |date=8 August 1929|title=L'avion léger Muniz M.5|journal=Les Ailes|issue=425 |pages=3|url=http://gallica.bnf.fr/ark:/12148/bpt6k65546552/f3 }}
3. ^{{cite journal |date=7 August 1930|title=Les premièrs' vols de l'avion Muniz M-5|journal=Les Ailes|issue=477 |pages=9|url=http://gallica.bnf.fr/ark:/12148/bpt6k65537449/f9 }}
4. ^{{cite journal |date=8 January 1931|title=D'aérodrome en aérodrome - à Villacoubly|journal=Les Ailes|issue=499 |pages=12|url=http://gallica.bnf.fr/ark:/12148/bpt6k6555748k/f12 }}
5. ^{{cite journal |date=21 April 1932|title=Petites nouvelles|journal=Les Ailes|issue=566 |pages=12|url=http://gallica.bnf.fr/ark:/12148/bpt6k6560162h/f15.item.r=Muniz.zoom }}
6. ^{{cite journal |date=8 August 1929 |title=International light plane tour of Europe|journal= Flight |volume=XXI|issue=32|pages=845| url=https://www.flightglobal.com/pdfarchive/view/1929/1929-1%20-%200700.html }}
[1][2][3][4][5][6]
}}{{Muniz aircraft}}

2 : Brazilian civil aircraft 1930–1939|Muniz aircraft

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