Yayınlar & Eserler

Yayın Ağı
Makaleler 12
Tümü (12)
SCI-E, SSCI, AHCI (12)
SCI-E, SSCI, AHCI, ESCI (12)
Scopus (12)

1. Improved combustion model of boron particles for ducted rocket combustion chambers

Kalpakli B., Acar E. B., ULAŞ A.
COMBUSTION AND FLAME , cilt.179, ss.267-279, 2017 (SCI-Expanded, Scopus) identifier identifier

2. Characterization of BPN Pyrotechnic Composition Containing Micro- and Nanometer-Sized Boron Particles

Koc S., ULAŞ A., Yilmaz N. E.
PROPELLANTS EXPLOSIVES PYROTECHNICS , cilt.40, sa.5, ss.735-742, 2015 (SCI-Expanded, Scopus) identifier identifier

3. Two dimensional numerical prediction of deflagration-to-detonation transition in porous energetic materials

Narin B., ÖZYÖRÜK Y., ULAŞ A.
JOURNAL OF HAZARDOUS MATERIALS , cilt.273, ss.44-52, 2014 (SCI-Expanded, Scopus) identifier identifier identifier

4. Numerical analysis of regenerative cooling in liquid propellant rocket engines

ULAŞ A., Boysan E.
AEROSPACE SCIENCE AND TECHNOLOGY , cilt.24, sa.1, ss.187-197, 2013 (SCI-Expanded, Scopus) identifier identifier

5. Calculation of Detonation Properties of Gaseous Explosives Using Generalized Reduced Gradient Nonlinear Optimization

ULAŞ A., Cengiz F.
PROPELLANTS EXPLOSIVES PYROTECHNICS , cilt.36, sa.4, ss.314-319, 2011 (SCI-Expanded, Scopus) Sürdürülebilir Kalkınma identifier identifier

6. A numerical study on the thermal initiation of a confined explosive in 2-D geometry

Aydemir E., ULAŞ A.
JOURNAL OF HAZARDOUS MATERIALS , cilt.186, sa.1, ss.396-400, 2011 (SCI-Expanded, Scopus) identifier identifier identifier

7. An experimental study on the hypergolic ignition of hydrogen peroxide and ethanolamine

Ak M. A., ULAŞ A., Sumer B., Yazici B., Yildirim C., Gonc L. O., et al.
FUEL , cilt.90, sa.1, ss.395-398, 2011 (SCI-Expanded, Scopus) identifier identifier

8. Numerical prediction of steady-state detonation properties of condensed-phase explosives

Cengiz F., ULAŞ A.
JOURNAL OF HAZARDOUS MATERIALS , cilt.172, ss.1646-1651, 2009 (SCI-Expanded, Scopus) identifier identifier identifier

9. 3-D grain burnback analysis of solid propellant rocket motors: Part 1-ballistic motor tests

Puskulcu G., ULAŞ A.
AEROSPACE SCIENCE AND TECHNOLOGY , cilt.12, sa.8, ss.579-584, 2008 (SCI-Expanded, Scopus) identifier identifier

10. 3-D grain burnback analysis of solid propellant rocket motors: Part 2-modeling and simulations

Puskulcu G., ULAŞ A.
AEROSPACE SCIENCE AND TECHNOLOGY , cilt.12, sa.8, ss.585-591, 2008 (SCI-Expanded, Scopus) identifier identifier

11. Laser-induced ignition of solid propellants for gas generators

ULAŞ A., Kuo K. K.
FUEL , cilt.87, sa.6, ss.639-646, 2008 (SCI-Expanded, Scopus) identifier identifier

12. An investigation of the performance of a boron/potassium-nitrate based pyrotechnic igniter

Ulas A., Risha G. A., Kuo K. K.
PROPELLANTS EXPLOSIVES PYROTECHNICS , cilt.31, sa.4, ss.311-317, 2006 (SCI-Expanded, Scopus) identifier identifier
Hakemli Bilimsel Toplantılarda Yayımlanmış Bildiriler 16

1. Design Methodology for a Central Injection Type Supersonic Air Ejector and Diffuser System for Altitude Simulation

aydoğdu a., sümer b., yazıcı b., ULAŞ A.
AIAA Propulsion and Energy 2019 Forum, Indianapolis, Amerika Birleşik Devletleri, 19 - 22 Ağustos 2019, (Tam Metin Bildiri) identifier

2. Investigation of the Effect of Geometrical Parameters of Pressure Swirl Atomizer on the Hollow Cone Spray

tokgöz t., sümer b., ULAŞ A.
AIAA Propulsion and Energy 2019 Forum, Indianapolis, Amerika Birleşik Devletleri, 19 - 22 Ağustos 2019, (Tam Metin Bildiri) identifier

3. Evaluation of an Augmented Spark Igniter’s Flame Length and Comparison of Numerical and Experimental Investigations

Öz L., Özer A. C., Sümer B., ULAŞ A.
AIAA Propulsion and Energy 2019 Forum, Indianapolis, Amerika Birleşik Devletleri, 19 - 22 Ağustos 2019, (Tam Metin Bildiri) identifier

4. Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants

Özcan S., cürdaneli s., ULAŞ A.
2018 AIAA Propulsion and Energy Forum, cincinnati, Amerika Birleşik Devletleri, 9 - 11 Temmuz 2018, (Tam Metin Bildiri)

5. Ballistic Performance of BPN Igniter Compositions Containing Micron and Nano-Sized Boron Particles

Koç S., Eroğul Kombe F., ULAŞ A.
53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, GA, Amerika Birleşik Devletleri, 10 - 12 Temmuz 2017, (Tam Metin Bildiri)

6. Design and Testing of a Green Bipropellant Thruster for Satellite Propulsion

Yılmaz Ç., Bayramoğlu M., Göçmen M., ULAŞ A.
53rd AIAA/SAE/ASEE Joint Propulsion Conference, Atlanta, GA, Amerika Birleşik Devletleri, 10 - 12 Temmuz 2017, (Tam Metin Bildiri)

7. A Test Bench for Gas Turbine Combustor Cooling Investigations

inanlı s., YASA T., ULAŞ A.
12th international conference on heat transfer fluid mechanics and thermodynamics, 11 - 13 Temmuz 2016, (Tam Metin Bildiri)

8. Experimental Investigation of Effusion and Film Cooling for Gas Turbine Combustor

inanlı s., YASA T., ULAŞ A.
12th international conference on heat traansfer fluid mechanics and thermodynamics, 11 - 13 Temmuz 2016, (Tam Metin Bildiri)

9. Comparison of BPN Igniter Compositions Containing Micron and Nano Sized Boron Particles

Koç S., ULAŞ A.
51st AIAA/SAE/ASEE Joint Propulsion Conference, 27 - 29 Temmuz 2015, (Tam Metin Bildiri)

10. Application of parallel processing to numerical modeling of two-phase deflagration-to-detonation (DDT) phenomenon

Bekir B., ÖZYÖRÜK Y., ULAŞ A.
Parallel Computational Fluid Dynamics, Parallel CFD 2007, Antalya, Türkiye, 21 - 24 Mayıs 2007, ss.123-130, (Tam Metin Bildiri) identifier

11. 1 D two phase modeling of deflagration to detonation transition DDT phenomenon in porous energetic materials

NARİN B., ÖZYÖRÜK Y., ULAŞ A.
AIAC'2007 Ankara International Aerospace Conference, Ankara, Turkey, 10 - 12 Eylül 2007, (Tam Metin Bildiri)

12. Comparison of different aspect ratio cooling channel designs for a liquid propellant rocket engine

Boysan M. E., ULAŞ A., Toker K. A., Seckin B.
3rd International Conference on Recent Advances in Space Technologies, İstanbul, Türkiye, 14 - 16 Haziran 2007, ss.225-226, (Tam Metin Bildiri) identifier identifier

13. Experimental analysis on the measurement of ballistic properties of solid propellants

Cuerdaneli S., Ak M. A., ULAŞ A.
3rd International Conference on Recent Advances in Space Technologies, İstanbul, Türkiye, 14 - 16 Haziran 2007, ss.231-232, (Tam Metin Bildiri) identifier identifier

14. Development of one dimensional solver for two phase reactive deflagration to detonation transition phenomenon in porous energetic materials

NARİN B., ÖZYÖRÜK Y., ULAŞ A.
AIAC'2005 Ankara International Aerospace Conference, Ankara, Turkey, 22 - 25 Ağustos 2005, (Tam Metin Bildiri)

15. EFFECTS OF FLUORINE-CONTAINING SPECIES ON THE IGNITION AND COMBUSTION OF BORON PARTICLES: EXPERIMENT AND THEORY

ULAŞ A., Kuo K. K., Gotzmer C.
The Fifth International Symposium on Special Topics in Chemical Propulsion, stresa, İtalya, 18 - 22 Haziran 2000, ss.453-463, (Tam Metin Bildiri)

16. Combustion of HTPB-based solid fuels containing nano-sized energetic powder in a hybrid rocket motor

Risha G., ULAŞ A., Boyer E., Kumar S., Kuo K. K.
37th Joint Propulsion Conference and Exhibit, Salt Lake City,UT,U.S.A., 8 - 11 Temmuz 2001, (Tam Metin Bildiri)
Metrikler

Yayın

28

Yayın (WoS)

14

Yayın (Scopus)

18

Atıf (WoS)

190

H-İndeks (WoS)

9

Atıf (Scopus)

178

H-İndeks (Scopus)

8

Atıf (Scholar)

13

H-İndeks (Scholar)

1

Proje

3

Tez Danışmanlığı

28

Açık Erişim

17
BM Sürdürülebilir Kalkınma Amaçları