Roket angkasa

Roket angkasa

Bibliographic Details
Main Author:	FURNISS
Format:	Book
Language:	English
Published:	Kuala Lumpur Utusan Publications & Distributors 1991
Series:	Sri Teknologi Utusan
Subjects:	Rockets (Aeronautics)

Similar Items

Roket
Published: (1997)

Jane's all the world's aircraft, 2003-2004
Published: (2003)

Rockets and missiles
by: Gunston
Published: (1982)

Rockets and spacecraft how they work
by: Taylor
Published: (1959)

All the world's aircraft 2006-2007 ninety-seventh year of issue
Published: (2006)

Relativistic flight mechanics and space travel [electronic resource] a primer for students, engineers, and scientists
by: Tinder
Published: (2007)

Thunder over the horizon from V-2 rockets to ballistic missiles
by: Chun
Published: (2006)

Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow
by: Bashir, Musavir, et al.
Published: (2015)

Comparative analysis of alternative fuels in detonation combustion
by: Azami, Muhammad Hanafi, et al.
Published: (2016)

Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
by: Azami, Muhammad Hanafi, et al.
Published: (2019)

Rocket Propulsion Element George P. Sutton
by: SuttonhGeorge Paul
Published: (2010)

Guide to rockets, missiles, and satelites
by: Newell
Published: (1961)

Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges
by: Crasta, Asha, et al.
Published: (2015)

Nozzle expansion level effect on a suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)

Control of base pressure with micro jets:part-I
by: Rehman, Shafiqur, et al.
Published: (2008)

Control of suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)

Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012)

Stabilty derivatives in the newtonian limit
by: Crasta, Asha, et al.
Published: (2013)

Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
by: Crasta, Asha, et al.
Published: (2013)

CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows
by: Khan, Sher Afghan, et al.
Published: (2018)

Role of active control in increasing base pressure at Sonic Mach Number
by: G. M, Fharukh Ahmed, et al.
Published: (2019)

Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, et al.
Published: (2019)

Fundamentals of nuclear flight
by: Bussard
Published: (1965)

Effect of level of expansion and inertia level in a suddenly expanded flow
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)

Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2016)

Arbitrary Lagrangian-Eulerian Form of Flowfield Dependent Variation (ALE-FDV) Method for 3D Problems
by: Zulkifli, Mohammad, et al.
Published: (2014)

Effectiveness of micro-jets at different level of expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)

Inspection of supersonic flows in a CD nozzle using experimental method
by: Azami, Muhammad Hanafi, et al.
Published: (2019)

A BGK-based two-equation turbulence model algorithm for solving compressible navier-stokes equations
by: Ong, Jiunn Chit, et al.
Published: (2013)

Mechanics and Thermodynamics of Propulsion Philip G. Hill
by: Hill
Published: (1992)

Combined effect of relief and level of expansion in a suddenly expanded flow
by: Syed, Syed Ashfaq, et al.
Published: (2015)

Propeller test stand / Syed Khomeini Syed Hassan and Abd Manan Abd Rahman
by: Syed Hassan, Syed Khomeini, et al.
Published: (2004)

Roket gabus kutakluki angkasa
by: Nuriazam Ismail
Published: (2006)

The contribution of Hassan al-Rammah to gunpowder and rocket technology
by: Ahmed Ghazal, Belal, et al.
Published: (2011)

Active control of base pressure in suddenly expanded flow for area ratio 4.84
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)

Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
by: Ashfaq, Syed, et al.
Published: (2014)

Influence of micro jets on wall pressure for area ratio 3.24
by: Ashfaq, Syed, et al.
Published: (2014)

Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for mach 3.0 using CFD.
by: Quadros, Jaimon Dennis, et al.
Published: (2016)

Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, et al.
Published: (2016)