Mauboussin Hémiptère

{{Short description|1930s French experimental light aircraft}}

{{Infobox aircraft begin

| name=M.40 Hémiptère

| image=Mauboussin Hémiptère perspective drawing L'Aerophile May 1936.jpg

| caption=

}}{{Infobox aircraft type

| type=Experimental light aircraft

| national origin=France

| manufacturer=Avions Mauboussin

| designer=

| first flight=25 April 1936

| introduced=

| retired=1937

| status=

| primary user=

| more users=

| produced=

| number built=1

| program cost=

| unit cost=

| developed from=

| variants with their own articles=

}}

The Mauboussin M.40 Hémiptère was an experimental, single seat, single engine light aircraft with unequal span tandem wings, designed in France in the 1930s. Only one was built.

Design and development

Between 1928 and 1932 Pierre Mauboussin worked with Louis Peyret in the Peyret-Mauboussin concern before setting up on his own as Avions Mauboussin. Peyret had earlier designed a tandem wing glider which won first prize at the first British gliding competition in 1922. Despite the overlap of designers and the shared layout, Mauboussin's tandem winged Hémiptère was significantly different from Peyret's aerodynamically as well as being a powered aircraft. The journal Flight presumed that it was a reference to the insect order Hemiptera, whose hindwings are usually shorter than their forewings. This was also a feature of the Hémiptère, in contrast to the identical, swept wings of the Peyret glider.

Apart from its tandem wing, the Hémiptère was a conventional 1930s light aircraft, with a short, flat sided fuselage, a single open cockpit and a fixed tailskid undercarriage. It was powered by a nose-mounted (40 hp (30 kW) 4-cylinder Train engine. The front wing was mounted low on the fuselage and was unswept and of constant chord c = {{cvt|1.30|m}}, though with well rounded tips and with a generous trailing edge root fillet. It had about 1.5° of dihedral. The parallel chord rear wing had its leading edge exactly c behind the front wing's trailing edge. Mounted on the upper rear fuselage, it was just c/2 above the front wing. It had about two-thirds the span and 60% of the area of the front wing, with similar dihedral but a different, nearly symmetrical airfoil. It also had a lower angle of attack: viewing this tandem wing aircraft as a biplane with a large negative stagger of c, the decalage was -3°.

Due to its smaller area, lower angle of attack and more symmetrical airfoil, the rear wing generated less lift than the front; the interaction between the two wings also reduced the lift coefficient of the rear one compared with that of the same surface in isolation. Oval end plate fins recovered some of these losses and also carried rudders. Both wings carried pairs of control surfaces which acted together to control pitch. The front wing surfaces could also work together to act as lift generating flaps but did not move differentially as they had on the Peyret glider to provide roll control. The Hémiptère had ailerons only on the rear wing; the higher angle of attack, more asymmetric profile and the interaction between the two wings ensured that the front wing would stall first, leaving sufficient lateral control on the unstalled rear wing to avoid the spin. Wind tunnel tests suggested that the lower lift coefficient of the rear wing would require higher landing speeds than for conventional monoplane but that the tandem wing would have slightly lower drag at incidences up to about 10°.

The Hémiptère flew for the first time on 25 April 1935. It took part in the Rallye des vins de Touraine held on 1–19 July that year. Development was abandoned in 1937 in favour of other, more conventional, Mauboussin light aircraft designs.

Specifications

File:Mauboussin_Hémiptère_3-view_L'Aerophile_May_1936.jpg

{{Aircraft specs

|ref=AviaFrance

|prime units?=met

|genhide=

|crew=

|capacity=1

|length m=5.30

|length ft=

|length in=

|length note=

|span m=7.00

|span ft=

|span in=

|span note=

|height m=2.00

|height ft=

|height in=

|height note=

|wing area sqm=12.80

|wing area sqft=

|wing area note=including both wings

|aspect ratio=

|airfoil=

|empty weight kg=272

|empty weight lb=

|empty weight note=

|gross weight kg=399

|gross weight lb=

|gross weight note=

|max takeoff weight kg=

|max takeoff weight lb=

|max takeoff weight note=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=Train 4T

|eng1 type=4-cylinder inverted air-cooled inline

|eng1 kw=

|eng1 hp=40

|eng1 note=

|power original=

|thrust original=

|prop blade number=

|prop name=

|prop dia m=

|prop dia ft=

|prop dia in=

|prop note=

|perfhide=

|max speed kmh=160

|max speed mph=

|max speed kts=

|max speed note=

|max speed mach=

|cruise speed kmh=140

|cruise speed mph=

|cruise speed kts=

|cruise speed note=

|stall speed kmh=

|stall speed mph=

|stall speed kts=

|stall speed note=

|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=540

|range miles=

|range nmi=

|range note=

|combat range km=

|combat range miles=

|combat range nmi=

|combat range note=

|ferry range km=

|ferry range miles=

|ferry range nmi=

|ferry range note=

|endurance=

|ceiling m=3800

|ceiling ft=

|ceiling note=

|g limits=

|roll rate=

|glide ratio=

|climb rate ms=

|climb rate ftmin=

|climb rate note=

|time to altitude=

|sink rate ms=

|sink rate ftmin=

|sink rate note=

|lift to drag=

|wing loading kg/m2=

|wing loading lb/sqft=

|wing loading note=

|thrust/weight=

|more performance=

|avionics=

}}

{{aircontent

|see also=

|related=

|similar aircraft=

|lists=

}}

References

{{Commons category|Mauboussin M.40 Hémiptère}}

{{reflist|refs=

{{cite book |title= Jane's All the World's Aircraft 1938|last= Grey |first= C.G. |year=1938|publisher= David & Charles|location= London|isbn=0-7153-5734-4|page=129c }}

{{cite book |last= Grey |first= C.G.|title= Jane's All the World's Aircraft 1938 |page=56d }}

{{cite magazine |title=Reviving the Tandem|magazine= Flight|issue=17 November 1936 |page=293 |url= http://www.flightglobal.com/pdfarchive/view/1936/1936%20-%202533.html}}

{{cite web |url=http://www.aviafrance.com/mauboussin-m-40-hemiptere--aviation-france-9597.htm|title=Mauboussin M-40 Hémiptère |accessdate=2011-05-30}}

{{cite web |url=http://aeroplanedetouraine.fr/ephemerides/ephemeride-1936/|title=Rallye des vins de Touraine|accessdate=2011-05-31}}

{{cite web |url=http://richard.ferriere.free.fr/3vues/mauboussin_M40_3v.jpg|title=M.40 3-view|accessdate=2011-05-31}}

http://richard.ferriere.free.fr/3vues/mauboussin_M40_3v.jpg

http://aeroplanedetouraine.fr/ephemerides/ephemeride-1936/

}}

{{Mauboussin aircraft}}

{{DEFAULTSORT:Mauboussin Hemiptere}}

Category:Mauboussin aircraft

Category:1930s French civil aircraft

Category:Tandem-wing aircraft

Category:Single-engined tractor aircraft

Category:Aircraft first flown in 1936