FR2783499B1 - Avion supersonique a faible bang sonique et procedes de mise en oeuvre - Google Patents
Avion supersonique a faible bang sonique et procedes de mise en oeuvreInfo
- Publication number
- FR2783499B1 FR2783499B1 FR9811792A FR9811792A FR2783499B1 FR 2783499 B1 FR2783499 B1 FR 2783499B1 FR 9811792 A FR9811792 A FR 9811792A FR 9811792 A FR9811792 A FR 9811792A FR 2783499 B1 FR2783499 B1 FR 2783499B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- supersonic
- leading
- implementation
- methods
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/04—Influencing air flow over aircraft surfaces, not otherwise provided for by generating shock waves
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/04—Boundary layer controls by actively generating fluid flow
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/14—Boundary layer controls achieving noise reductions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/16—Boundary layer controls by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C2230/00—Boundary layer controls
- B64C2230/28—Boundary layer controls at propeller or rotor blades
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Lasers (AREA)
- Toys (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9811792A FR2783499B1 (fr) | 1998-09-22 | 1998-09-22 | Avion supersonique a faible bang sonique et procedes de mise en oeuvre |
FR9901619A FR2783496B1 (fr) | 1998-09-22 | 1999-02-11 | Rotors, soufflantes ou helices supersoniques a bon rendement et a faible bruit |
FR9901620A FR2783497B1 (fr) | 1998-09-22 | 1999-02-11 | Avion a aile supercritique a faible trainee d'onde |
FR9901621A FR2783498B1 (fr) | 1998-09-22 | 1999-02-11 | Turbo-reacteur a faible bruit au decollage et procedes de mise en oeuvre |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9811792A FR2783499B1 (fr) | 1998-09-22 | 1998-09-22 | Avion supersonique a faible bang sonique et procedes de mise en oeuvre |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2783499A1 FR2783499A1 (fr) | 2000-03-24 |
FR2783499B1 true FR2783499B1 (fr) | 2000-12-29 |
Family
ID=9530687
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9811792A Expired - Fee Related FR2783499B1 (fr) | 1998-09-22 | 1998-09-22 | Avion supersonique a faible bang sonique et procedes de mise en oeuvre |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2783499B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE10146121B4 (de) | 2001-09-19 | 2004-01-08 | Ford Global Technologies, Inc., Dearborn | Verfahren zur Bestimmung des Körperschall- und des Luftschallanteils eines Motorengeräusches |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3028129A (en) * | 1957-04-08 | 1962-04-03 | Faillie Andre Jean | Stream-lined aircraft body |
FR1195110A (fr) | 1958-04-24 | 1959-11-16 | Cellule à ailes parallèles pour avion supersonique | |
FR1558295A (fr) | 1967-06-27 | 1969-02-28 | ||
AT283826B (de) | 1968-02-14 | 1970-08-25 | Schoppe Fritz | Verfahren zur Verminderung der Intensität von Stoßwellen |
FR1569489A (fr) | 1968-06-25 | 1969-05-30 | ||
US4917335A (en) | 1988-03-31 | 1990-04-17 | Gt-Devices | Apparatus and method for facilitating supersonic motion of bodies through the atmosphere |
US5358156A (en) | 1990-07-23 | 1994-10-25 | Vehicle Research Corporation | Supersonic aircraft shock wave energy recovery system |
JPH04321489A (ja) * | 1991-04-19 | 1992-11-11 | Mitsubishi Heavy Ind Ltd | 航空機の翼 |
US5263661A (en) | 1992-09-11 | 1993-11-23 | Riley Jennifer K | Sonic boom attenuator |
-
1998
- 1998-09-22 FR FR9811792A patent/FR2783499B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2783499A1 (fr) | 2000-03-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |