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1.
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EFFECT OF INJECTION ELEMENT RADIAL DISTRIBUTION AND CHAMBER GEOMETRY ON ACOUSTIC-MODE INSTABILITY IN A HYDROGEN OXYGEN ROCKET
by Wanhainen,John P | Morgan,C Joe. Material type:  Book Description: 43.Publisher: Nasa, Washington, D.C. 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-5375 -] (1).
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2.
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EXPERIMENTAL INVESTIGATION OF ACOUSTIC LINERS TO SUPPRESS SCREECH IN HYDROGEN-OXYGEN ROCKETS
by Wanhainen,John P,Bloomer,Harry E | Vincent,David W. Material type: Book Description: 41.Publisher: Nasa, Washington, D.C. Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-3822] (1).
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3.
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NASA Technical Note [NASA TN D-4442]: Experimental investigation of acoustic liners to suppress screech in storable propellant rocket motors
by Washington. National Aeronautics and Space Administration (NASA) | Vincent, David W | Phillips, Bert | Wanhainen, John P. Description: 45p.Publisher: Washington NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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4.
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EFFECT OF CHAMBER PRESSURE, FLOW PER ELEMENT, AND CONTRACTION RATIO ON ACOUSTIC-MODE INSTABILITY IN HYDROGEN-OXYGEN ROCKETS
by Wanhainen,John P,Feiler,Charles E | Morgan,C Joe. Material type: Book Description: 35.Publisher: Nasa, Washington, D.C. 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4733] (1).
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5.
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INTERIM SUMMARY OF LIQUID ROCKET ACOUSTIC-MODE-INSTABILITY STUDIES AT A NOMINAL THRUST OF 20 000 POUNDS
by Conrad,E William,Bloomer,Harry E | Wanhainen,John P. Material type: Book Description: 90.Publisher: Nasa, Washington, D.C. 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4968] (1).
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6.
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Effect of propellant and catalyst bed temperatures on thrust buildup in several hydrogen peroxide reaction control rockets [NASA TN D-480]
by Wanhainen, John P | Ross, Phil S | DeWitt, Richard L. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 25p.Publisher: Washington, D. C. NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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7.
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NASA Technical Note: Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines
by Salmi, Reino J | Wanhainen, John P | Hannum, Ned P. Material type: Book Description: 27p.Publisher: Washington, D.C. NASA 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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8.
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Effect of injection element radial distribution and chamber geometry on acoustic mode instability in a hydrogen oxygen rocket [NASA TN D-5375]
by Wanhainen, John P. Material type: Book; Format:
print
; Literary form:
not fiction
Description: 43p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1969Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).
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