AT283826B - Verfahren zur Verminderung der Intensität von Stoßwellen - Google Patents
Verfahren zur Verminderung der Intensität von StoßwellenInfo
- Publication number
- AT283826B AT283826B AT140568A AT140568A AT283826B AT 283826 B AT283826 B AT 283826B AT 140568 A AT140568 A AT 140568A AT 140568 A AT140568 A AT 140568A AT 283826 B AT283826 B AT 283826B
- Authority
- AT
- Austria
- Prior art keywords
- intensity
- reducing
- shock waves
- waves
- shock
- Prior art date
Links
- 230000035939 shock Effects 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C30/00—Supersonic type aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Drilling And Exploitation, And Mining Machines And Methods (AREA)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT140568A AT283826B (de) | 1968-02-14 | 1968-02-14 | Verfahren zur Verminderung der Intensität von Stoßwellen |
| US792006*A US3620484A (en) | 1968-02-14 | 1969-01-17 | Method and structure for reduction of shock waves |
| GB7116/69A GB1255212A (en) | 1968-02-14 | 1969-02-10 | Method and structure for reduction of shock waves |
| FR6903550A FR2001895B1 (de) | 1968-02-14 | 1969-02-14 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AT140568A AT283826B (de) | 1968-02-14 | 1968-02-14 | Verfahren zur Verminderung der Intensität von Stoßwellen |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| AT283826B true AT283826B (de) | 1970-08-25 |
Family
ID=3513177
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT140568A AT283826B (de) | 1968-02-14 | 1968-02-14 | Verfahren zur Verminderung der Intensität von Stoßwellen |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US3620484A (de) |
| AT (1) | AT283826B (de) |
| FR (1) | FR2001895B1 (de) |
| GB (1) | GB1255212A (de) |
Families Citing this family (28)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4569494A (en) * | 1982-12-23 | 1986-02-11 | The Boeing Company | Pitch control of swept wing aircraft |
| US4790499A (en) * | 1984-07-31 | 1988-12-13 | Taylor Thomas C | Aerospike for attachment to space vehicle system |
| US4650139A (en) * | 1984-07-31 | 1987-03-17 | Taylor Thomas C | Aerospike for attachment to space vehicle system |
| US4917335A (en) * | 1988-03-31 | 1990-04-17 | Gt-Devices | Apparatus and method for facilitating supersonic motion of bodies through the atmosphere |
| FR2783499B1 (fr) | 1998-09-22 | 2000-12-29 | Gerard Fournier | Avion supersonique a faible bang sonique et procedes de mise en oeuvre |
| US7121511B2 (en) * | 2000-05-31 | 2006-10-17 | Kevin Kremeyer | Shock wave modification method and system |
| US7063288B1 (en) | 2000-05-31 | 2006-06-20 | Kevin Kremeyer | Shock wave modification method and system |
| US7648100B2 (en) * | 2000-05-31 | 2010-01-19 | Kevin Kremeyer | Shock wave modification method and system |
| US6527221B1 (en) * | 2000-05-31 | 2003-03-04 | Kevin Kremeyer | Shock wave modification method, apparatus, and system |
| US6404089B1 (en) * | 2000-07-21 | 2002-06-11 | Mark R. Tomion | Electrodynamic field generator |
| RU2271307C2 (ru) * | 2004-05-17 | 2006-03-10 | Владимир Александрович Иванов | Способ управления аэродинамическим обтеканием летательного аппарата и генератор плазмы |
| US7237752B1 (en) * | 2004-05-18 | 2007-07-03 | Lockheed Martin Corporation | System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping |
| RU2283794C2 (ru) * | 2004-06-22 | 2006-09-20 | Иркутский государственный университет | Способ управления обтеканием летательных аппаратов |
| RU2008109837A (ru) * | 2005-10-04 | 2009-11-20 | Сэйпоти БРУК (AU) | Система снижения лобового сопротивления и создания движущей и подъемной сил |
| US7407131B1 (en) * | 2005-11-14 | 2008-08-05 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Method for creating an aeronautic sound shield having gas distributors arranged on the engines, wings, and nose of an aircraft |
| JP2008002693A (ja) * | 2006-06-20 | 2008-01-10 | Japan Aerospace Exploration Agency | スパイク飛しょう体の空力特性制御方法およびスパイク飛しょう体 |
| DE102006028614B4 (de) * | 2006-06-22 | 2014-02-13 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zum Betrieb eines Strömungsflächenelements mit Plasmaerzeugungseinrichtungen |
| RU2343091C2 (ru) * | 2006-11-24 | 2009-01-10 | Государственное образовательное учреждение высшего профессионального образования Военно-космическая академия имени А.Ф. Можайского | Способ выведения воздушно-космического аппарата на околоземную орбиту |
| WO2009025803A1 (en) | 2007-08-20 | 2009-02-26 | Kevin Kremeyer | Energy-deposition systems, equipment and methods for modifying and controlling shock waves and supersonic flow |
| US8220753B2 (en) * | 2008-01-04 | 2012-07-17 | The Boeing Company | Systems and methods for controlling flows with pulsed discharges |
| US9446840B2 (en) * | 2008-07-01 | 2016-09-20 | The Boeing Company | Systems and methods for alleviating aircraft loads with plasma actuators |
| US8473267B2 (en) * | 2009-03-31 | 2013-06-25 | Airbus Operations, S.L. | Computer-aided method for a cost-optimized calculation of variable distributions over an aerodynamic surface |
| RU2422336C1 (ru) * | 2009-10-26 | 2011-06-27 | Дмитрий Геннадьевич Белянин | Способ создания теплового канала для вывода воздушно-космического аппарата на околоземную орбиту с помощью "пушечного" старта |
| US10669653B2 (en) | 2015-06-18 | 2020-06-02 | Kevin Kremeyer | Directed energy deposition to facilitate high speed applications |
| US10435135B2 (en) | 2015-09-02 | 2019-10-08 | Charl E. Janeke | System, apparatus and methods for hypersonic shockwave muffler |
| US10023329B1 (en) * | 2017-03-04 | 2018-07-17 | Othniel Mbamalu | Space vehicle system |
| US10928168B2 (en) * | 2017-11-10 | 2021-02-23 | Curtis E. Graber | Noise control system and method for small caliber ammunition |
| CN111392026A (zh) * | 2020-03-23 | 2020-07-10 | 南京航空航天大学 | 一种高超声速飞行器头锥主动热防护系统 |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB635784A (en) * | 1946-07-19 | 1950-04-19 | Zygmurit Stefan Jablonski | Apparatus for reducing fluid friction |
| US2995317A (en) * | 1955-09-14 | 1961-08-08 | Metallbau Semler G M B H | External combustion stato-jet engine |
| US3028129A (en) * | 1957-04-08 | 1962-04-03 | Faillie Andre Jean | Stream-lined aircraft body |
| US2949550A (en) * | 1957-07-03 | 1960-08-16 | Whitehall Rand Inc | Electrokinetic apparatus |
| US3259065A (en) * | 1959-04-30 | 1966-07-05 | Massachusetts Inst Technology | Shock wave inducing means for supersonic vehicles |
| US3446464A (en) * | 1967-03-09 | 1969-05-27 | William A Donald | Method and apparatus for reducing sonic waves and aerodynamic drag |
-
1968
- 1968-02-14 AT AT140568A patent/AT283826B/de not_active IP Right Cessation
-
1969
- 1969-01-17 US US792006*A patent/US3620484A/en not_active Expired - Lifetime
- 1969-02-10 GB GB7116/69A patent/GB1255212A/en not_active Expired
- 1969-02-14 FR FR6903550A patent/FR2001895B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1255212A (en) | 1971-12-01 |
| FR2001895B1 (de) | 1973-11-16 |
| FR2001895A1 (de) | 1969-10-03 |
| US3620484A (en) | 1971-11-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| ELJ | Ceased due to non-payment of the annual fee |